AIAA JOURNAL OF PROPULSION AND POWER

AIAA JOURNAL OF PROPULSION AND POWER http://www.aiaa.org/Research/index.hfm?res=13 Volume 19 Number 5 September 2003 Combustion Dynamics in Lean-Premixed Prevaporized (LPP) Gas Turbines Introduction: Combustion Dynamics in Lean-Premixed Prevaporized (LPP) Gas Turbines Tim Lieuwen; Keith McManus Combustion Dynamics and Instabilities: Elementary Coupling and Driving Mechanisms Sébastien Ducruix; Thierry Schuller; Daniel Durox; Sébastien Candel Experimental Diagnostics for the Study of Combustion Instabilities in Lean Premixed Combustors J. G. Lee; D. A. Santavicca Acoustic Analysis of Gas Turbine Combustors Ann P. Dowling; Simon R. Stow Modeling Premixed Combustion-Acoustic Wave Interactions: A Review T. Lieuwen Large-Eddy Simulation of Combustion Dynamics of Lean-Premixed Swirl-Stabilized Combustor Ying Huang; Hong-Gye Sung; Shih-Yang Hsieh; Vigor Yang Passive Control of Combustion Dynamics in Stationary Gas Turbines Geo A. Richards; Douglas L. Straub; Edward H. Robey Factors Affecting the Control of Unstable Combustors Jeffrey M. Cohen; Andrzej Banaszuk Challenges and Progress in Controlling Dynamics in Gas Turbine Combustors H. C. Mongia; T. J. Held; G. C. Hsiao; R. P. Pandalai Full-length Papers Time-Averaged Gradient Control of Thermoacoustic Instabilities Michael A. Vaudrey; William T. Baumann; William R. Saunders Premixed Flame Kinematics in a Longitudinal Acoustic Field Doh-Hyoung Lee; Tim C. Lieuwen Atomic Emission Spectrometry for Profiling High Temperatures in Combustion System Shigeo Yatsu; Hiroyuki Oyama; Takunari Mizuno; Hideharu Kimura; Kuniyuki Kitagawa; Naoyuki Kayukawa Ignition Characteristics of Methane and Hydrogen Using a Plasma Torch in Supersonic Flow Tomoaki Kitagawa; Atsushi Moriwaki; Koichi Murakami; Kenichi Takita; Goro Masuya 853 847 837 830 822 811 795 782 765 751 735 722 721 Conceptual Study of a Combined-Cycle Engine for an Aerospace Plane Takeshi Kanda; Kenji Kudo Aerodynamic Performance Analysis of a Hypersonic Inlet Isolator Using Computation and Experiment Birgit U. Reinartz; Carsten D. Herrmann; Josef Ballmann; Wolfgang W. Koschel Effects of Injection Configuration on Performance of a Staged Supersonic Combustor Sadatake Tomioka; Kan Kobayashi; Kenji Kudo; Atsuo Murakami; Tohru Mitani Fuel Injection and Flame Stabilization in a Liquid-Kerosene-Fueled Supersonic Combustor G. Yu; J. G. Li; X. Y. Chang; L. H. Chen; C. J. Sung Magnetohydrodynamic Power Generation Experiments with Fuji-1 Blowdown Facility Y. Okuno; T. Okamura; T. Suekane; H. Yamasaki; S. Kabashima; S. Shioda Some Aspects of Chemical Kinetics in Chapman-Jouguet Detonation: Induction Length Analysis Tianfeng Lu; Chung K. Law; Yiguang Ju Partial Fuel Filling in Pulse Detonation Engines Chiping Li; K. Kailasanath Tailored Fuel Injection for Pulsed Detonation Engines via Feedback Control Alberto Aliseda; Kartik B. Ariyur; Olivier Sarrazin; Juan C. Lasheras; Miroslav Krstic Two-Dimensional Compressible Non-Acoustic Modeling of Stirling Machine-Type Components Roy C. Tew Jr; Mounir B. Ibrahim Jet Engine Gas-Path Measurement Filtering Using Center Weighted Idempotent Median Filters Ranjan Ganguli Dynamic and Nonlinear Simulation of Liquid-Propellant Engines H. Karimi; A. Nassirharand Multi-Element Unstructured Methodology for Analysis of Turbomachinery Systems Vineet Ahuja; Jeremy D. Shipman; S. Arunajatesan; Ashvin Hosangadi Numerical Parameter Studies of Ion-Thruster-Beam Neutralization Carsten Othmer; Karl-Heinz Glassmeier; Uwe Motschmann; Ingo Richter Development of a Finite Element-Based Hall-Thruster Model Subrata Roy; B. P. Pandey Volume 19 Number 4 July 2003 Full-length Papers 859 868 876 885 894 901 908 917 922 930 938 945 953 964 Analysis of Inducer Recirculating Inlet Flow François Bario; Thierry M. Faure; Emmanuel Jondeau; Jean-Luc Normand; Jean-Michel Nguyen Duc Theoretical Performance of a Magnetohydrodynamic-Bypass Scramjet Engine with Nonequilibrium Ionization Chul Park; David W. Bogdanoff; Unmeel B. Mehta Deceleration of Supersonic Plasma Flow by an Applied Magnetic Field Sergei V. Bobashev; Yurii P. Golovachov; David M. Van Wie Computational Fluid Dynamics Analysis of the Central Institute of Aviation Motors/NASA Scramjet Carlos G. Rodriguez System Performance and Thermodynamic Cycle Analysis of Airbreathing Pulse Detonation Engines Yuhui Wu; Fuhua Ma; Vigor Yang Pulse Detonation Engine Characterization and Control Using Tunable Diode-Laser Sensors Daniel W. Mattison; Christopher M. Brophy; Scott T. Sanders; Lin Ma; Kevin M. Hinckley; Jay B. Jeffries; Ronald K. Hanson Detonation Initiation by Controlled Triggering of Electric Discharges S. M. Frolov; V. Y. Basevich; V. S. Aksenov; S. A. Polikhov Constant-Frequency Hypervelocity Slings D. A. Tidman Measurements and Simulation of Orifice Flow for Micropropulsion Testing A. A. Alexeenko; S. F. Gimelshein; D. A. Levin; A. D. Ketsdever; M. S. Ivanov One-Dimensional Hollow Cathode Model Ira Katz; John R. Anderson; James E. Polk; John R. Brophy Ignition Delay for Jet Propellant 10/Air and Jet Propellant 10/HighEnergy Density Fuel/Air Mixtures David W. Mikolaitis; Corin Segal; Abhilash Chandy Numerical Simulation of Ion Beam Optics for Multiple-Grid Systems Yoshinori Nakayama; Paul J. Wilbur Combustion and Thermal Studies on Al/Ti/Ni/Zr Composite Modified Double-Base Systems C. N. Divekar; S. N. Asthana; Haridwar Singh Erosive Burning of Ammonium Perchlorate/Hydroxyl-TerminatedPolybutadiene Propellants Under Supersonic Crossflows S. Krishnan; K. K. Rajesh Characteristics of Liquid Film and Spray Injected from Swirl Coaxial Injector Takao Inamura; Hiroshi Tamura; Hiroshi Sakamoto Analytical and Experimental Studies of Tile-Shaped Aerospike Nozzles 521 529 538 547 556 568 573 581 588 595 601 607 614 623 632 640 Wu-Ye Dai; Yu Liu; Xian-Chen Cheng; Bin Ma Closed-Loop Vectoring Control of a Turbulent Jet Using Periodic Excitation D. Rapoport; I. Fono; K. Cohen; A. Seifert Flow Separation Inside a Supersonic Nozzle Exhausting into a Subsonic Compressible Crossflow S. J. Beresh; J. F. Henfling; R. J. Erven Improved Aerodynamic-Ramp Injector in Supersonic Flow L. S. Jacobsen; S. D. Gallimore; J. A. Schetz; W. F. O'Brien Rotordynamic Bearing Dampers for Cryogenic Rocket Engine Turbopumps Bugra H. Ertas; Eyad Al-Khateeb; John M. Vance Evaluating Experimental Data Requirements for Spatially Varying Turbine Flowfields Through Uncertainty Analysis Susan T. Hudson; Boon Liang Heng Adjoint Calculation of Sensitivities of Turbomachinery Objective Functions M. Sergio Campobasso; Mihai C. Duta; Michael B. Giles Low-Engine-Order Excitation Mechanisms in Axial-Flow Turbomachinery C. Bréard; J. S. Green; M. Imregun Technical Notes Combustion Effects of C60 Soot in Ammonium Nitrate Propellants Brian E. Greiner; Robert A. Frederick Jr.; Marlow D. Moser Performance Analysis of Short Takeoff and Vertical Landing Aircraft Nozzle in Hover Frank K. Lu; Douglas A. Terrier Erratum Errata on Theoretical Performance of Frictionless Magnetohydrodynamics-Bypass Scramjet Chul Park; David Bogdanoff; Unmeel B. Mehta Volume 19 Number 3 May 2003 Full-length Papers Scalability for Rocket Nozzle Flows Based on Subscale and Full-Scale Testing Gerald Hagemann; Jan Alting; Dieter Preclik Edge Diffusion Flame Stabilization Behind a Step over a Liquid Reactant Matthew Juniper; Sébastien Candel Characterization of Cryogenic Injection at Supercritical Pressure Richard Branam; Wolfgang Mayer 342 332 321 718 715 713 704 693 683 674 663 655 646 Improvement of Inlet Flow Characteristics of LE-7A Liquid Hydrogen Pump Masaharu Uchiumi; Kenjiro Kamijo; Kunio Hirata; Akira Konno; Tomoyuki Hashimoto; Satoshi Kobayasi Rocket Engine Turbine Blade Surface Pressure Distributions: Experiment and Computations Susan T. Hudson; Thomas F. Zoladz; Daniel J. Dorney Effect of Nozzle Cavity on Resonance in Large SRM: Numerical Simulations J. Anthoine; J.-M. Buchlin; J.-F. Guéry Two-Phase Vorticoacoustic Flow Interactions in Solid-Propellant Rocket Motors Weidong Cai; Fuhua Ma; Vigor Yang Thermoviscoelastic Characterization of a Composite Solid Propellant Using Tubular Test V. R. Sanal Kumar Constant Volume Explosions of Aerosols of Metallic Mechanical Alloys and Powder Blends Mirko Schoenitz; Edward L. Dreizin; Emil Shtessel Optimization of Electric Thrusters for Primary Propulsion Based on the Rocket Equation Monika Auweter-Kurtz; Helmut Kurtz Model of an Electrothermal Pulsed Plasma Thruster Michael Keidar; Iain D. Boyd; Isak I. Beilis Scale Effects on Solid-Propellant Coaxial Magnetoplasmadynamic Thruster Performance Giorgio Paccani; Luigi Petrucci; William D. Deininger Low-Current, Xenon Orificed Hollow Cathode Performance for In-Space Applications Matthew T. Domonkos; Michael J. Patterson; Alec D. Gallimore Conservation Coupling Technique for Dynamic Inlet-Engine Analyses Keith Numbers; Awatef Hamed Multicriteria Design Optimization of Integrated Three-Dimensional Supersonic Inlets Arnaud Gaiddon; Doyle D. Knight Normal Shock/Boundary-Layer Interaction Control Using Aeroelastic Mesoflaps Everett S. Hafenrichter; Yeol Lee; J. Craig Dutton; Eric Loth Computation of Transonic Diffuser Flows by a Lagged k-_ Turbulence Model Q. Xiao; H. M. Tsai; F. Liu Characteristics and Control of Combustion Instabilities in a SwirlStabilized Spray Combustor S. Acharya; S. Murugappan; M. O'Donnell; E. J. Gutmark 356 364 374 385 397 405 413 424 431 438 444 456 464 473 484 Study of Interspacecraft Coulomb Forces and Implications for Formation Flying Lyon B. King; Gordon G. Parker; Satwik Deshmukh; Jer-Hong Chong Hysteresis Effects on Thrust Measurement and its Uncertainty Joseph D. Sims; Hugh W. Coleman Technical Notes Analysis of Entrainment in a Sudden-Expansion Channel with Wall Mass Transfer Jing-Tang Yang; Shih-Chao Lee; Yei-Chin Chao Leading-Edge Shape and Aeroengine Fan Blade Performance A. I. Sayma; M. Kim; N. H. S. Smith 497 506 514 517 Volume 19 Number 2 March 2003 Full-length Papers Conceptual Development of Quiet Turbofan Engines for Supersonic Aircraft Dimitri Papamoschou; Marco Debiasi Integration of an Aeroramp Injector/Plasma Igniter for Hydrocarbon Scramjets L. S. Jacobsen; S. D. Gallimore; J. A. Schetz; W. F. O'Brien Operational Sensitivities of an Integrated Scramjet Ignition/FuelInjection System S. D. Gallimore; L. S. Jacobsen; W. F. O'Brien; J. A. Schetz High Ram Acceleration Using Open-Base Projectile Yuichiro Hamate; Akihiro Sasoh; Kazuyoshi Takayama Kinetic Model for Aluminum-Sensitized Ram Accelerator Combustion Laurent Catoire; Jean-François Legendre; Marc Giraud Study of Combustion Characteristics of Ammonium Dinitramide/Polycaprolactone Propellants Oleg P. Korobeinichev; Alexander A. Paletsky; Alexander G. Tereschenko; Evgeny N. Volkov Design and Use of a Batch Reactor for Catalytic Decomposition of Propellants Rachel Eloirdi; Sylvie Rossignol; Charles Kappenstein; Daniel Duprez; Nicolas Pillet Stability of Hydrogen/Hydrocarbon Blended Fuel Flames Ahsan R. Choudhuri; S. R. Gollahalli Numerical Simulation of High-Pressure and Fuel-Rich Turbulent Combustion Field Takurou Makita; Takahisa Yamamoto; Tomohiko Furuhata; Norio Arai Two-Phase Computational Fluid Dynamics Analysis Applied to Prefilming Pure-Airblast Atomizer 235 226 220 213 203 196 190 183 170 161 Philip E. O. Buelow; Chien-Pei Mao; Steven Smith; David Bretz Axial Compressor Blade-to-Blade Unsteady Aerodynamic Variability Douglas M. Boyd; Sanford Fleeter Effects of Flow Instabilities on the Linear Analysis of Turbomachinery Aeroelasticity M. Sergio Campobasso; Michael B. Giles Numerical Simulation of Aerodynamic Damping for Flutter Analysis of Turbomachinery Blade Rows R. Srivastava; M. A. Bakhle; T. G. Keith Jr. Proper Orthogonal Decomposition of Turbine Rotor-Stator Interaction Paul G. A. Cizmas; Antonio Palacios Inlet/Engine Interactions in an Axisymmetric Pulse Detonation Engine System Jonas Gustavsson; Venkata Nori; Corin Segal Vortex Shedding Induced Sound Inside a Cold-Flow Simulation of Segmented Chamber Alison Flatau; W. K. Van Moorhem Numerical Simulations of Wall and Shear Layer Instabilities in Cold Flow Setup Jérôme Vétel; Frédéric Plourde; Son Doan Kim; Jean-François Guery Technical Notes Analyzing Mistuning of Bladed Disks by Symmetry and Reduced-Order Aerodynamic Modeling B. Shapiro; K. E. Willcox Active Control of Compressor Instability and Surge by Stator Blades Adjustment M. T. Schobeiri; M. Attia Aerodynamic Design of a VerticalThrust Adapter for Jet Engines T. Strand Volume 19 Number 1 January 2003 Editorial Announcements and Acknowledgments Reviewers for October 2001-September 2002 Ethical Standards for Publication of Aeronautics and Astronautics Research AIAA Manuscript Review Process Full-length Papers Assessing Jet-Induced Spatial Mixing in a Rich, Reacting Crossflow T. N. Demayo; M. Y. Leong; G. S. Samuelsen; J. D. Holdeman Analytical Model for the Impulse of Single-Cycle Pulse Detonation Tube 22 14 1 11 12 13 317 312 307 297 287 282 268 260 250 242 E. Wintenberger; J. M. Austin; M. Cooper; S. Jackson; J. E. Shepherd Thrust-Vectoring Nozzle Performance Modeling Erich A. Wilson; Dan Adler; Pinhas Bar-Yoseph Numerical Simulation of Distributed Combustion in Solid Rocket Motors with Metalized Propellant Jayant S. Sabnis Plateau Burning Behavior of Ammonium Perchlorate Sandwiches and Propellants at Elevated Pressures Satyanarayanan R. Chakravarthy; Edward W. Price; Robert K. Sigman; Jerry M. Seitzman Optical Fouling of the RB199 Pyrometer Clive Kerr; Paul Ivey Bypass-Regulated Solid Fuel Ramjet Combustor in Variable Flight Conditions Deborah Pelosi-Pinhas; Alon Gany Investigation of Instabilities in a Lean, Premixed Step Combustor Jeffrey M. Cohen; Brian E. Wake; Dochul Choi Sensitivity of Hydrocarbon Combustion Modeling for Hypersonic Missile Design Ryan P. Starkey; Mark J. Lewis Rocketdyne Hypersonic Flow Laboratory as High-Performance Expansion Tube for Scramjet Testing Benjamin S. Stewart; Richard G. Morgan; Peter A. Jacobs Sonic Injection from Diamond-Shaped Orifices into a Supersonic Crossflow Sadatake Tomioka; Lance S. Jacobsen; Joseph A. Schetz Mixing Augmentation of Transverse Injection in Scramjet Combustor Sang-Hyeon Lee; Tohru Mitani Combined/Simultaneous Gust and Oscillating Compressor Blade Unsteady Aerodynamics Kuk Kim Frey; Sanford Fleeter Traveling Wave Excitation System for Bladed Disks Keith W. Jones; Charles J. Cross Numerical Study of Cryogenic Jets Under Supercritical Conditions J. M. M. Barata; A. R. R. Silva Technical Notes Optimal Actuator/Sensor Placement for Control of Combustion Instabilities Nidal Al-Masoud; Tarunraj Singh Modified Mixing Analogy for Studies of Mixing in Supersonic Flows Sadatake Tomioka; Lance S. Jacobsen; Joseph A. Schetz Technical Comments 151 148 142 135 125 115 104 98 89 81 73 66 56 48 39 Technical Comment on "Vorticity Dynamics in Isobarically Closed Porous Channels, Part 1: Standard Perturbations," R. L. Glick Reply to Robert L. Glick's Comment: Physicality of Core Flow Models in Rocket Motors Joseph Majdalani 155 156 Volume 18 Number 6 November 2002 Advanced Performance Modeling of Experimental Laser Lightcraft Ten-See Wang; Yen-Sen Chen; Jiwen Liu; Leik N. Myrabo; Franklin B. Mead Jr. Analysis and Application of Chorochronic Periodicity in Turbomachinery Rotor/Stator Interaction Computations G. A. Gerolymos; G. J. Michon; J. Neubauer Experimental Study of the Transient Underexpanded Jet Generated by Electrothermal Capillary Plasma Jong-Uk Kim; N. T. Clemens; P. L. Varghese Mass-Based Optimization of Thermal Management and Power Systems for Space Applications K. D. Freudenberg; W. E. Lear; S. A. Sherif; E. L. Golliher Thermodynamics of Airbreathing Pulse-Detonation Engines J. A. C. Kentfield Thermodynamic Limits of Work and Pressure Gain in Combustion and Evaporation Processes M. Razi Nalim Work Potential Perspective of Engine Component Performance Bryce Roth Numerical Reconstruction of Ejector Rocket Experimental Tests A. Matesanz; A. Velazquez; J. Tizon; J. Montanes Motor and Plume Particle Size Prediction in Solid-Propellant Rocket Motors Oleg B. Kovalev Casting Process Impact on Small-Scale Solid Rocket Motor Ballistic Performance P. Le Breton; D. Ribéreau Comparison of Laser- and Pressure-Driven Thrust Response of HMX Gautam N. Kudva; Thomas A. Litzinger Modeling Cavitating Venturi Flows Changhai Xu; Stephen D. Heister; Robert Field Hydrogen Peroxide Decomposition on Various Supported Catalysts Effect of Stabilizers Laurence Pirault-Roy; Charles Kappenstein; Maurice Guérin; Rachel Eloirdi; Nicolas Pillet 1235 1227 1218 1211 1199 1191 1183 1176 1170 1161 1153 1139 1129 Thermochemistry of Species Produced from Monomethylhydrazine in Propulsion and Space-Related Applications Laurent Catoire; Mark T. Swihart Advanced Seals for Industrial Turbine Applications: Design Approach and Static Seal Development Mahmut F. Aksit; Raymond E. Chupp; O. Saim Dinc; Mehmet Demiroglu Advanced Seals for Industrial Turbine Applications: Dynamic Seal Development Raymond E. Chupp; Farshad Ghasripoor; Norman A. Turnquist; Mehmet Demiroglu; Mahmut F. Aksit Measured Flow Oscillations and Instabilities in Labyrinth Seal Cavities David L. Rhode; J. Wayne Johnson Effects of Blade Count on Linearized and Nonlinear Hot Streak Clocking Simulations Douglas L. Sondak; Vipul Gupta; Paul D. Orkwis; Daniel J. Dorney Airfoil Row/Wake Interactions in a High-Speed Axial Compressor Robert T. Johnston; Sanford Fleeter Interaction of Decaying Freestream Turbulence with a Moving Shock Wave: Pressure Field S. Xanthos; G. Briassulis; Y. Andreopoulos Proportional Control of Combustion Instabilities in a Simulated GasTurbine Combustor Christian Oliver Paschereit; Ephraim Gutmark Technical Notes Effects of End Wall Geometry and Stacking on Supersonic Turbine Performance Daniel J. Dorney; Lisa W. Griffin; Frank W. Huber; Douglas L. Sondak Controlling Electron Backstreaming Phenomena Through the Use of a Transverse Magnetic Field John E. Foster; Michael J. Patterson 2002 Journal of Propulsion and Power Index Subject Index Author Index Chronological Index Volume 18 Number 5 September 2002 Full-Length Papers A PIV Investigation of Rotor-IGV Interactions in a Transonic Compressor Albert J. Sanders; John Papalia; Sanford Fleeter Turbomachine Blade Row Interaction Predictions with a ThreeDimensional Finite Element Method Dana A. Gottfried; Sanford Fleeter 1242 1254 1260 1267 1273 1280 1289 1298 1305 1308 1312 1318 1320 969 978 Analysis of Dual-Mode Hydrocarbon Scramjet Operation at Mach 46.5 R. A. Baurle; D. R. Eklund Acoustic Flutter Control of Three-Dimensional Transonic Rotor Flow Pong-Jeu Lu; Dartzi Pan; Yi-Di Yu High-Speed Centrifugal Compressor Surge Initiation Characterization William C. Oakes; Patrick B. Lawless; John R. Fagan; Sanford Fleeter Gas Turbine Engine and Sensor Fault Diagnosis Using Optimization Techniques Marco Zedda; Riti Singh Effect of Integration of Scramjet into Airframe on Engine Performance and Payload Daisuke Akihisa; Takeshi Kanda; Kouichiro Tani; Kenji Kudo; Goro Masuya Direct Experimental Impulse Measurements for Detonations and Deflagrations M. Cooper; S. Jackson; J. Austin; E. Wintenberger; J. E. Shepherd Numerical Simulation of a Pulse Detonation Engine with Hydrogen Fuels Houshang B. Ebrahimi; Charles L. Merkle Influence of Radical Concentration and Fuel Decomposition on Ignition of Propane/Air Mixture Yuriy Ya. Buriko; Viacheslav A. Vinogradov; Valentin F. Goltsev; Paul J. Waltrup Effects of Halons and Halon Replacements on Hydrogen-Fueled Laminar Premixed Flames C. H. Kim; O. C. Kwon; G. M. Faeth Pilot Flame Effects on Gas Jet Flames in Crossflow Sien-Fong Goh; S. R. Gollahalli Assessment of Combustion Characteristics and Mechanism of Hydroxylammonium Nitrate-Based Liquid Monopropellant Yi-Ping Chang; Kenneth K. Kuo Nonlinear Heterogeneous Model of Composite Solid-Propellant Combustion B. Rasmussen; R. A. Frederick Jr. Combustion Response of Ammonium Perchlorate Composite Propellants Michael Shusser; Fred E. C. Culick; Norman S. Cohen Property Transformation of Thermotropic Liquid Crystals Polymers J. J. Rusek; K. P. Chaffee High Strain-Rate Constitutive Models for Solid Rocket Propellants Sook-Ying Ho Study of Flow Separation in Truncated Ideal Contour Nozzle S. B. Verma 990 1003 1012 1019 1026 1033 1042 1049 1059 1068 1076 1086 1093 1101 1106 1112 Technical Notes Experimental Investigation of End-Wall Flow in Turbine Rotor X. Xiao; B. Lakshminarayana Effect of Transient Gasdynamic Processes on the Impulse of Pulse Detonation Engines C. B. Kiyanda; V. Tanguay; A. J. Higgins; J. H. S. Lee Supersonic Wave/Blade-Row Interactions Establish Boundary Conditions for Unsteady Inlet Flows Miklos Sajben 1126 1124 1122 Volume 18 Number 4 July 2002 Special Section: Electric Propulsion Space Experiment (ESEX) Program Electric Propulsion Space Experiment (ESEX) Roger M. Myers Review of the Electric Propulsion Space Experiment (ESEX) Program D. R. Bromaghim; J. R. Leduc; R. M. Salasovich; G. G. Spanjers; J. M. Fife; M. J. Dulligan; J. H. Schilling; D. C. White; L. K. Johnson System Engineering, Design, Integration, and Qualification of Electric Propulsion Space Experiment Mary M. Kriebel Development and Flight Qualification of a 26-Kilowatt Arcjet Propulsion Subsystem R. J. Cassady; W. A. Hoskins; C. E. Vaughan Orbital Performance Measurements of Air Force Electric Propulsion Space Experiment Ammonia Arcjet J. M. Fife; D. R. Bromaghim; D. A. Chart; W. A. Hoskins; C. E. Vaughan; L. K. Johnson Effect of ESEX 26-kW Arcjet Operation on Spacecraft Communications M. J. Dulligan; R. Bromaghim; J. A. Zimmerman; R. M. Salasovich; D. Hardesty; L. K. Johnson On-Orbit Optical Observations of Electric Propulsion Space Experiment 26-Kilowatt Arcjet L. K. Johnson; G. G. Spanjers; D. R. Bromaghim; M. W. Dulligan; W. A. Hoskins Solar Cell Degradation During the 26-Kilowatt Electric Propulsion Space Experiment Flight J. H. Schilling; G. G. Spanjers; D. R. Bromaghim; L. K. Johnson Mass Deposition Measurements from 26-Kilowatt Electric Propulsion Space Experiment Flight G. G. Spanjers; J. H. Schilling; S. F. Engelman; D. R. Bromaghim; L. K. Johnson Radiometric Analysis from the 26-Kilowatt Electric Propulsion Space Experiment Flight p777 p772 p768 p763 p754 p749 p740 p731 p723 p721 G. G. Spanjers; J. H. Schilling; D. R. Bromaghim; L. K. Johnson Full-Length Papers Observations of Soot in the Combustion of Methanol/Toluene Spray Flames C. T. Avedisian; C. Presser; A. K. Gupta Computational-Fluid-Dynamics Investigation of Aeromechanics Peter D. Silkowski; Chae M. Rhie; George S. Copeland; James A. Eley; James M. Bleeg Facility Effects on Performance Measurements of Micropropulsion Systems that Utilize Gas Expansion Andrew D. Ketsdever Sensitivity of Solid Rocket Motors to Electrostatic Discharge: History and Future Alain Davenas; Roger Rat Announcements and Acknowledgments Asphaltic Thermoplastic Propellants John J. Rusek Full-Length Papers Model of Aluminum Agglomerate Evolution in Combustion Products of Solid Rocket Propellant V. A. Babuk; V. A. Vasilyev Chemical Speciation and Dynamics in the Surface Combustion Zone of Energetic Materials Thomas B. Brill; Merrill C. Beckstead; Joseph E. Flanagan; M. C. Lin; Thomas A. Litzinger; R. H. Woodward Waesche; Charles A. Wight Thermomechanical Analysis and Optimization of Cryogenic Liquid Rocket Engines Detlef Kuhl; Jörg Riccius; Oskar J. Haidn Effect of Momentum Ratio on the Mixing Performance of Unlike Split Triplet Injectors Y. D. Won; Y. H. Cho; S. W. Lee; W. S. Yoon Flourescence and Temperature Measurements in an Actively Forced Swirl-Stabilized Spray Combustor V. Santhanam; F. C. Knopf; S. Acharya; E. Gutmark Heat Release Rates of Burning Items in Fires Hyeong-Jin Kim; David G. Lilley New Fossil Power Systems and the Role of Open-Cycle Magnetohydrodynamics Generators Naoyuki Kayukawa Application of Autoassociative Neural Network on Gas-Path Sensor Data Validation Pong-Jeu Lu; Tzu-Cheng Hsu Control of Low-Pressure Turbine Separation Using Vortex-Generator Jets p889 p879 p871 p866 p855 p847 p835 p824 p814 p810 p805 p797 p788 p781 Rolf Sondergaard; Richard B. Rivir; Jeffrey P. Bons Analysis and Multidisciplinary Optimization of Internal Coolant Networks in Turbine Blades Thomas J. Martin; George S. Dulikravich Optimum Mixing of Core and Bypass Streams in High-Bypass Civil Turbofan Vivek Sanghi; B. K. Lakshmanan; S. K. Sane Automated Design Optimization of a Three-Dimensional S-Shaped Subsonic Diffuser Sophia Lefantzi; Doyle D. Knight Inlet/Compressor System Response to Short-Duration Acoustic Disturbances Anthony B. Opalski; Miklos Sajben Analysis of a Fusion-Electric Airbreathing Earth to Orbit Launch Vehicle Robert B. Adams; D. Brian Landrum Characterization of Expansion Tube Flows for Hypervelocity Combustion Studies Adela Ben-Yakar; Ronald K. Hanson Drag and Total Pressure Distributions in Scramjet Engines at Mach 8 Flight Tohru Mitani; Tetsuo Hiraiwa; Yuichi Tarukawa; Goro Masuya Technical Notes Laser-Air Interactions in an Internal Supersonic Flowpath Robert B. Adams; D. Brian Landrum Timescaling Control Volumes During Real Time Digital Simulation of a Military Turbofan Vivek Sanghi; B. K. Lakshmanan Technical Comments Comment on "Equation for Additive Drag Coefficient at Static Conditions" William H. Heiser; Jack D. Mattingly Reply to Technical Comment from William H. Heiser and Jack D. Mattingly K. L. Christensen Volume 18 Number 3 May 2002 Full-Length Papers Project Orion and Future Prospects for Nuclear Pulse Propulsion G. R. Schmidt; J. A. Bonometti; C. A. Irvine Study of the Phase-Lock Phenomenon for a Circular Slingatron G. R. Cooper; D. A. Tidman Shape Optimization of Supersonic Turbines Using Global Approximation Methods 509 505 497 p968 p967 p964 p961 p953 p943 p933 p922 p913 p907 p896 Approximation Methods Nilay Papila; Wei Shyy; Lisa Griffin; Daniel J. Dorney Unsteady Cascade Aerodynamics in the Time Domain Dana A. Gottfried; Sanford Fleeter Multiobjective Optimization of Rocket Engine Pumps Using Evolutionary Algorithm Akira Oyama; Meng-Sing Liou Three-Dimensional Hybrid Mesh Generation for Turbomachinery Airfoils Kyu-Sup Kim; Paul G. A. Cizmas Development of High-Performance Airfoils for Axial Flow Compressors Using Evolutionary Computation Ernesto Benini; Andrea Toffolo High-Pressure Steam Flow in Turbine Bypass Valve System Part 1: Valve Flow R. S. Amano; G. R. Draxler High-Pressure Steam Flow in Turbine Bypass Valve System Part 2: Pipe Flow R. S. Amano; G. R. Draxler; J. M. Golembiewski Acceptance Screening of Turbopump Gears Using the Cepstrum Method S. J. DiMaggio Appearance of Restricted Shock Separation in Rocket Nozzles G. Hagemann; M. Frey; W. Koschel Performance Analysis of Secondary Gas Injection into a Conical Rocket Nozzle Hyun Ko; Woong-Sup Yoon Ejector Primary Flow Molecular Weight Effects in an Ejector-Ram Rocket Engine Sam Han; John Peddieson Jr.; David Gregory Solid-Fuel Regression Rate Behavior of Vortex Hybrid Rocket Engines William H. Knuth; Martin J. Chiaverini; J. Arthur Sauer; Daniel J. Gramer Combustion of Liquefying Hybrid Propellants: Part 1, General Theory M. A. Karabeyoglu; D. Altman; B. J. Cantwell Combustion of Liquefying Hybrid Propellants: Part 2, Stability of Liquid Films M. A. Karabeyoglu; B. J. Cantwell Burning Aluminum Particles Inside a Laboratory-Scale Solid Rocket Motor John C. Melcher; Herman Krier; Rodney L. Burton Evaluation of Ultrasound Technique for Solid-Propellant Burning-Rate Response Measurements Jeffrey J. Murphy; Herman Krier 641 631 621 610 600 592 585 577 572 561 555 544 536 528 519 Aerodynamic Optimization of Turbomachinery Cascades Using Euler/Boundary-Layer Coupled Genetic Algorithms Ozhan Oksuz; I. Sinan Akmandor; Mehmet S. Kavsaoglu When Do Open-Loop Strategies for Combustion Control Work? R. K. Prasanth; A. M. Annaswamy; J. P. Hathout; A. F. Ghoniem Flashover: A Study of Parameter Effects on Time to Reach Flashover Conditions Hyeong-Jin Kim; David G. Lilley Comparison of Criteria for Room Flashover Hyeong-Jin Kim; David G. Lilley Effects of Airstream Mach Number on H2/N2 Plasma Igniter Goro Masuya; Kenichi Takita; Katsuyoshi Takahashi; Fumio Takatori; Hiroyuki Ohzeki Elliptic Coflow Effects on a Circular Gas Jet Flame Ahsan R. Choudhuri; Sayela P. Luna; S. R. Gollahalli Experimental Study of a 3-kW Stirling Engine Noboru Kagawa Improved Mean-Flow Solution for Slab Rocket Motors with Regressing Walls Chong Zhou; Joseph Majdalani Technical Notes Geometric Evaluation of Axisymmetric Thrust-Vectoring Nozzles for Aerodynamic Performance Predictions Erich A. Wilson; Dan Adler; Pinhas Z. Bar-Yoseph Combustion Characteristics of Ethylene in Scramjet Engines A. A. Taha; S. N. Tiwari; T. O. Mohieldin High-Intensity Sound Absorption at an Orifice with Bias Flow Xiaodong Jing; Xiaofeng Sun Volume 18 Number 2 March 2002 Full-Length Papers Multilevel Analysis of Pulsed Detonation Engines Houshang B. Ebrahimi; Rajendran Mohanraj; Charles L. Merkle Development of Advanced Industrial Furnace Using Highly Preheated Combustion Air T. Hasegawa; S. Mochida; A. K. Gupta Effects of Liquid-Oxygen Post Biasing on SSME Injector Wall Compatibility P. A. Strakey; D. G. Talley; L. K. Tseng; K. I. Miner Time- and Length Scales of Combustion in Liquid Rocket Thrust Chambers B. Ivancic; W. Mayer 652 658 669 674 679 686 696 703 712 716 718 225 233 240 247 Computations of Axisymmetric Plug-Nozzle Flowfields: Flow Structures and Thrust Performance Takashi Ito; Kozo Fujii; A. Koich Hayashi Numerical Simulation of Side Loads in an Ideal Truncated Nozzle Sébastien Deck; Philippe Guillen Design Analysis of a Satellite Hydrazine Propulsion System An-Shik Yang; Tien-Chuan Kuo Leak Fault Detection of Liquid Rocket Engine Based on Strong Tracking Filter Yu Daren; Wang Jianbo Temperature-Dependent Modal Test/Analysis Correlation of X-34 FASTRAC Composite Rocket Nozzle Andrew M. Brown Characteristic Analysis of Flow-Induced Vibrations on Inducer of Oxygen Pump Liang Hengli; Chen Zuoyi Numerical Predictions of Channel Flows with Fluid Injection Using Reynolds-Stress Model Bruno Chaouat Effect of Nozzle Cavity on Resonance in Large SRM: Theoretical Modeling J. Anthoine; J-M. Buchlin; A. Hirschberg Dynamic Combustion of Solid Propellants: Effects of Unsteady Condensed Phase Degradation Layer K. R. Anil Kumar; K. N. Lakshmisha Slingatron: A High Velocity Rapid Fire Sling Derek A. Tidman Sizing a Slingatron-Based Space Launcher Mark L. Bundy; Derek A. Tidman; Gene R. Cooper Numerical Simulations of the Slingatron G. R. Cooper; D. A. Tidman; M. L. Bundy Ethylene Ignition and Detonation Chemistry, Part 1: Detailed Modeling and Experimental Comparison B. Varatharajan; F. A. Williams Ethylene Ignition and Detonation Chemistry, Part 2: Ignition Histories and Reduced Mechanisms B. Varatharajan; F. A. Williams Study of the High-Temperature Autoignition of n-Alkane/O2/Ar Mixtures D. C. Horning; D. F. Davidson; R. K. Hanson Profiling of Redox Index During Combustion to Monitor C/C Composite Degradation in Flames Kuniyuki Kitagawa; Masao Kubota; Norio Arai; Ashwani K. Gupta Chemiluminescence-Based Feedback Control of Equivalence Ratio for a Continuous Combustor 254 261 270 280 284 289 295 304 312 322 330 338 344 352 363 372 376 a Continuous Combustor Douglas A. Scott; Galen B. King; Normand M. Laurendeau Linear Deterministic Source Terms for Hot Streak Simulations Paul D. Orkwis; Mark G. Turner; John W. Barter Combustion Instability Active Control Using Periodic Fuel Injection J. P. Hathout; M. Fleifil; A. M. Annaswamy; A. F. Ghoniem Constant Volume Limit of Pulsed Propulsion for a Constant _ Ideal Gas Douglas G. Talley; Edward B. Coy Combustion Air Jet Influence on Primary Zone Characteristics for GasTurbine Combustors S. Gogineni; D. Shouse; C. Frayne; J. Stutrud; G. Sturgess Mach 8 Testing of a Scramjet Engine with Ramp Compression Takeshi Kanda; Kouichiro Tani; Kan Kobayashi; Toshihito Saito; Tetsuji Sunami Magnetohydrodynamic Power Extraction from Cold Hypersonic Airflows with External Ionizers Sergey O. MacHeret; Mikhail N. Shneider; Richard B. Miles Analysis of a High-Efficiency Low-Emissions "Chemical Gas Turbine" System Takahisa Yamamoto; Tomohiko Furuhata; Norio Arai; Noam Lior Fuzzy Logic Intelligent System for Gas Turbine Module and System Fault Isolation Ranjan Ganguli Particle Image Velocimetry Characterization of a Chordwise Bending Cascade Flowfield Daniel A. Ehrlich; Sanford Fleeter Rotor Blade-to-Blade Wake Variability and Effect on Downstream Vane Response Albert J. Sanders; Sanford Fleeter Massively Parallel Simulation of the Unsteady Flow in an Axial Turbine Stage Jixian Yao; Roger L. Davis; Juan J. Alonso; Antony Jameson Impeller Blade Unsteady Aerodynamic Response to Vaned Diffuser Potential Fields Dana Gottfried; Sanford Fleeter Recent GRC Aerospace Technologies Applicable to Terrestrial Energy Systems M. David Kankam; Valerie J. Lyons; Mark A. Hoberecht; Robert R. Tacina; Aloysius F. Hepp Technical Notes Correlating Laser Induced Fluorescence and Molecular Beam Mass Spectrometry Ion Energy Distributions George J. Williams; Timothy B. Smith; Frank S. Gulczinski; Alec D. Gallimore 489 481 472 465 456 448 440 432 424 417 407 400 390 383 Transonic Rotor Blade Pressure Measurement Using Fluorescent Paints T. Liu; S. Torgerson; J. Sullivan; R. Johnston; S. Fleeter Unsteady Flow in a Supersonic Turbine with Variable Specific Heats Daniel J. Dorney; Lisa W. Griffin; Frank Huber; Douglas L. Sondak Volume 18 Number 1 January 2002 Editorial Announcements and Acknowledgments V. Yang Reviewers for October 2000-September 2001 Editorial Policy Statement on Numerical Accuracy and Experimental Uncertainty Ethical Standards for Publication of Aeronautics and Astronautics Research AIAA Manuscript Review Process Full-Length Papers History of U.S. Navy Ramjet, Scramjet, and Mixed-Cycle Propulsion Development P. J. Waltrup; M. E. White; F. Zarlingo; E. S. Gravlin Integrated Design and Analysis of Intakes and Nozzles in Air-Breathing Engines M. Ferlauto; F. Larocca; L. Zannetti Analytical Model of the Base Flow Between a Subsonic and Supersonic Flow Doo S. Baik; Glen W. Zumwalt Numerical Simulation of the Ram Accelerator Using a New Chemical Kinetics Mechanism Michael J. Nusca Scale-Up Experiments on Liquid-Fueled Active Combustion Control Ken H. Yu; Ken J. Wilson Experimental Investigation of Limit-Cycle Oscillations in an Unstable Gas Turbine Combustor Tim C. Lieuwen Thermodynamic Cycle Analysis of Pulse Detonation Engines William H. Heiser; David T. Pratt Fundamentals of Idealized Airbreathing Pulse-Detonation Engines J. A. C. Kentfield Selection of Actuators and Sensors for Surge Control Marc Van De Wal; Frank Willems; Bram De Jager Flow Control via Rotor Trailing Edge Blowing in Rotor/Stator Axial Compressor 491 493 1 10 11 12 13 14 28 35 44 53 61 68 77 84 93 A. M. Wo; A. C. Lo; W. C. Chang Active Control of Discrete-Frequency Noise Generated by Rotor-Stator Interactions Scott Sawyer; Sanford Fleeter; John Simonich Shock Fitting a Transonic Cascade Solution into an Inverse Design Technique Jeffrey W. Yokota; Adam J. Medd Experimental and Analytical Design Verification of the Dual-Bell Concept Gerald Hagemann; Michael Terhardt; Dietrich Haeseler; Manuel Frey Effects of Grain Geometry on Pulse-Triggered Combustion Instability in Rocket Motors Mehdi Golafshani; Mohammad Farshchi; Hojat Ghassemi Overview of the Development of Hydrazinium Nitroformate H. F. R. Schöyer; W. H. M. Welland-Veltman; J. Louwers; P. A. O. G. Korting; A. E. D. M. van der Heijden; H. L. J. Keizers; R. P. van den Berg Overview of the Development of Hydrazinium Nitroformate-Based Propellants H. F. R. Schöyer; W. H. M. Welland-Veltmans; J. Louwers; P. A. O. G. Korting; A. E. D. M. van der Heijden; H. L. J. Keizers; R. P. van den Berg Design of a Fusion Propulsion System - Part 1: Gigawatt-Level Magnetoplasmadynamic Source Pavlos G. Mikellides; Peter J. Turchi; Ioannis G. Mikellides Design of a Fusion Propulsion System - Part 2: Numerical Simulation of Magnetic-Nozzle Flows Ioannis G. Mikellides; Pavlos G. Mikellides; Peter J. Turchi; Thomas M. York Interior and Exterior Laser-Induced Fluorescence and Plasma Measurements within a Hall Thruster W. A. Hargus Jr; M. A. Cappelli Verification Tests of Carbon-Carbon Composite Grids for Microwave Discharge Ion Thruster I. Funaki; H. Kuninaka; K. Toki; Y. Shimizu; K. Nishiyama; Y. Horiuchi Cascade Arc Studies of Hydrogen/Nitrogen Plasmas in Nonequilibrium Trevor Moeller; Dennis Keefer; Robert Rhodes Flow Past Stationary Spherical Particles with Streamwise Velocity Fluctuation A. Dasgupta; T. I-P. Shih Reduced Chemical Kinetic Mechanisms for Hydrocarbon Fuels Christopher J. Montgomery; Marc A. Cremer; Jyh-Yuan Chen; Berkeley Berkeley; Charles K. Westbrook; Lourdes Q. Maurice Two-Dimensional Spectroscopic Analysis of a Flame Using Highly Preheated Combustion Air Noriyuki Konishi; Kuniyuki Kitagawa; Norio Arai; Ashwani K. Gupta 199 192 184 176 169 159 152 146 138 131 123 116 107 100 Technical Notes Anomalous Deflagration Behavior of Ammonium Perchlorate at Elevated Pressures Satyanarayanan R. Chakravarthy; Edward W. Price; Robert K. Sigman; Jeffrey M. Freeman Effects of GH2/LOX Velocity and Momentum Ratios on Shear Coaxial Injector Atomization M. Ferraro; R. J. Kujala; J.-L. Thomas; M. J. Glogowski; M. M. Micci Equation for Additive Drag Coefficient at Static Conditions K. L. Christensen Intercusp Electron Transport in an NSTAR-Derivative Ion Thruster John E. Foster Optimal Three-Dimensional Nozzle Shape Design Using CFD and Parallel Simulated Annealing X. Wang; M. Damodaran Propagation of Acoustic Waves in a Two-Phase Vaporizing Mixture Joël Dupays; François Vuillot Erratum Progress in Hypersonic Science and Technology Development Volume 17 Number 6 November 2001 Editorial History Scramjet Engines: The First Forty Years Edward T. Curran Program Overview and Case Studies Two-Stage-to-Orbit Spaceplane Concept with Growth Potential Unmeel B. Mehta; Jeffrey V. Bowles Testing Technologies and Flight Experiments Numerical Research of Gaseous Fuel Preinjection in Hypersonic Three-Dimensional Inlet O. V. Guoskov; V. I. Kopchenov; K. E. Lomkov; V. A. Vinogradov; P. J. Waltrup Program Overview and Case Studies Development of Hydrocarbon-Fueled Scramjet Engines: The Hypersonic Technology (HyTech) Program O. A. Powell; J. T. Edwards; R. B. Norris; K. E. Numbers; J. A. Pearce French-Russian Partnership on Hypersonic Wide-Range Ramjets Marc Bouchez; François Falempin; Vadim Levine; Valery Avrashkov; Dmitri Davidenko Multidisciplinary Optimization of Airbreathing Hypersonic Vehicles Kevin G. Bowcutt 1184 1177 1170 1162 1149 1138 1137 224 222 217 213 211 209 205 Synthesis of a FESTIP Airbreathing TSTO Space Transportation System H. Grallert System Performance Analysis and Concept Studies Upper Bounds on the Flight Speed of Hydrocarbon-Fueled ScramjetPowered Vehicles Paul J. Waltrup Domain of the Scramjet L. H. Townend Significance of Fuel Selection for Hypersonic Vehicle Range Mark J. Lewis Structural Mechanics and Materials Experimental Study of Scramjet Module Marat A. Goldfeld; Alexey V. Starov; Viacheslav V. Vinogradov System Performance Analysis and Concept Studies Strutjet Engine Performance Bryan T. Campbell; Adam Siebenhaar; Thong Nguyen Structural Mechanics and Materials Development Study of a Precooler for the Air-Turboramjet ExpanderCycle Engine Kenya Harada; Nobuhiro Tanatsugu; Tetsuya Sato Combined Engine for Reusable Launch Vehicle (KLIN Cycle) V. V. Balepin; P. A. Czysz; R. H. Moszée Advancement of Scramjet Magnetohydrodynamic Concept B. M. Burakhanov; A. P. Likhachev; S. A. Medin; V. A. Novikov; V. I. Okunev; V. Yu. Rickman; V. A. Zeigarnik Fundamental Mechanisms: Combustion and Fuel Management Initiators for Endothermic Fuels D. T. Wickham; J. R. Engel; B. D. Hitch; M. E. Karpuk 1191 1199 1205 1214 1222 1227 1233 1239 1247 1253 Thermal Stability of Energetic Hydrocarbon Fuels for Use in Combined 1258 Cycle Engines K. Wohlwend; L. Q. Maurice; T. Edwards; R. C. Striebich; M. Vangsness; A. S. Hill Investigation of Kerosene Combustion Characteristics with Pilot Hydrogen in Model Supersonic Combustors G. Yu; J. G. Li; X. Y. Chang; L. H. Chen; C. J. Sung Historical Survey on Enhanced Mixing in Scramjet Engines John M. Seiner; S. M. Dash; D. C. Kenzakowski Effect of Flame-Holding Cavities on Supersonic-Combustion Performance Ken H. Yu; Ken J. Wilson; Klaus C. Schadow Newly Developed Direct-Connect High-Enthalpy Supersonic Combustion Research Facility 1296 1287 1273 1263 Combustion Research Facility Mark Gruber; Jeffrey Donbar; Kevin Jackson; Tarun Mathur; Robert Baurle; Dean Eklund; Charles Smith Supersonic Combustion Experiments with a Cavity-Based Fuel Injector Tarun Mathur; Mark Gruber; Kevin Jackson; Jeff Donbar; Wayne Donaldson; Thomas Jackson; Fred Billig Dual-Mode Combustion of Hydrogen in a Mach 5, Continuous-Flow Facility C. P. Goyne; J. C. McDaniel; T. M. Quagliaroli; R. H. Krauss; S. W. Day Numerical Simulation of Supersonic Airflow with Transverse Hydrogen Injection E. von Lavante; D. Zeitz; M. Kallenberg Effects of Swirl and Skew Upon Supersonic Wall Jet in Crossflow A. D. Cutler; S. E. Doerner Skin-Friction Measurements in a Supersonic Combustor with Crossflow Fuel Injection H. Tanno; A. Paull; R. J. Stalker Thermal Analysis of Fluid-Structural Interaction in High-Speed Engine Flowfields Birgit U. Reinartz; Wolfgang W. Koschel Fundamental Mechanisms: Inlet and Nozzle Optimal Design of Plug Nozzles and Their Thrust Determination at Start A. N. Kraiko; N. I. Tillyayeva; S. V. Baftalovskii Computation of a Nonequilibrium Expansion Flow in a Single Expansion Ramp Nozzle Thomas Link; Wolfgang W. Koschel Testing Technologies and Flight Experiments Experimentation, Test, and Evaluation Requirements for Future Airbreathing Hypersonic Systems Dan Marren; Mark Lewis; Lourdes Q. Maurice Quasi-One-Dimensional High-Speed Engine Model with Finite-Rate Chemistry Timothy F. O'Brien; Ryan P. Starkey; Mark J. Lewis Volume 17 Number 5 September 2001 Full-Length Papers Hybrid (Particle-Fluid) Modeling of Pulsed Plasma Thruster Plumes Nikolaos A. Gatsonis; Xuemin Yin Heating and Plasma Properties in a Coaxial Gasdynamic Pulsed Plasma Thruster Stewart S. Bushman; Rodney L. Burton 959 945 1366 1361 1353 1347 1339 1333 1327 1319 1313 1305 Quasi-Steady Magnetoplasmadynamic Thruster Performance Database E. Y. Choueiri; J. K. Ziemer Electrospray as a Source of Nanoparticles for Efficient Colloid Thrusters M. Gamero-Castaño; V. Hruby Impact of Energy Gain and Subsystem Characteristics on Fusion Propulsion Performance S. Chakrabarti; G. R. Schmidt Development of a Resonance Igniter for GO2/Kerosene Ignition Mario Niwa; A. Santana Jr.; Khoze Kessaev Nonlinear Control of a Reusable Rocket Engine for Life Extension Carl F. Lorenzo; Asok Ray; Michael S. Holmes Flame-Spreading Phenomena in Fin Slots of a Solid Rocket Motor K. K. Kuo; R. A. Kokal; M. Paulauskas; P. Alaksin; L. S. Lee Effects of Oxidizer Particle Size on Propellants Based on Modified Polyvinyl Chloride Vladica S. Bozic; Marko V. Milos Burning-Rate Modifier Effects on a Modified Polyvinyl Chloride-Based Propellants Vladica S. Bozic; Djordje Dj. Blagojevic Development of Thermal Barriers for Solid Rocket Motor Nozzle Joints Bruce M. Steinetz; Patrick H. Dunlap Jr. Flexibilized Novolac Epoxy Resin for Inhibition of Composite Propellants J. P. Agrawal; N. T. Agawane Russian Research on Experimental Hydrogen-Fueled Dual-Mode Scramjet: Conception and Preflight Tests Donat A. Ogorodnikov; Viacheslav A. Vinogradov; Yurii M. Shikhman; Vitaliy N. Strokin Magnetohydrodynamics Energy Bypass Scramjet Performance with Real Gas Effects Chul Park; Unmeel B. Mehta; David W. Bogdanoff Ignition and Flame Studies for an Accelerating Transonic Mixing Layer X. Fang; F. Liu; W. A. Sirignano Underexpanded Jet for Testing Laser-Based Combustion Diagnostics K. G. Klavuhn; J. C. McDaniel Effect of Ambient Pressure on an Airblast Spray Injected into a Crossflow May Y. Leong; Vincent G. McDonell; G. Scott Samuelsen Ignition Delays in MMH + CH4 + O2 + Ar Mixtures Laurent Catoire; Gabrielle Dupré; Claude Paillard; Abdelkrim Elaissi Acoustic-Wave/Blade-Row Interactions Establish Boundary Conditions for Unsteady Inlet Flows 967 977 988 995 998 1005 1012 1017 1023 1035 1041 1049 1058 1067 1076 1085 1090 for Unsteady Inlet Flows Miklos Sajben; Hazem Said Mechanisms and Prediction Methods for Fan Blade Stall Flutter M. Vahdati; A. I. Sayma; J. G. Marshall; M. Imregun Experimental Investigation of Lobed Mixer Performance A. Abolfadl; M. A. Metwally; A. M. El-Messiry; M. A. Ali Optimum Fan Pressure Ratio for Bypass Engines with Separate or Mixed Exhaust Streams Abhijit Guha Optimization of Turbomachinery Airfoils with a Genetic/ SequentialQuadratic-Programming Algorithm Brian H. Dennis; George S. Dulikravich; Zhen-Xue Han Technical Notes Mixing of Supersonic Jets in a Strutjet Propulsion System S. Muller; Clark W. Hawk; P. G. Bakker; D. Parkinson; M. Turner Modular Ignition System Based on Resonance Igniter M. Niwa; A. Santana Jr.; K. Kessaev Experimental Investigation of Pulsatile Flow in Circular Tubes Josef Adamec; Ji í No i ka; Daniel Hanus; Josef Ko ená Volume 17 Number 4 July 2001 Full-Length Papers Direct Flight to Pluto Using Solar Electric Propulsion J. S. Meserole; W. R. Richards Low Mass Components for Mars Ascent Propulsion Keith Dyer; George Yankura; Jesus Acosta Triple Langmuir Probe Measurements in the Plume of a Pulsed Plasma Thruster Robert Eckman; Lawrence Byrne; Nikolaos A. Gatsonis; Eric J. Pencil Computation of Hall Thruster Performance L. Garrigues; I. D. Boyd; J. P. Boeuf High-Pressure Bipropellant Microrocket Engine A. P. London; A. H. Epstein; J. L. Kerrebrock Experimental Study of Major Species and Temperature Profiles of Liquid Oxygen/Gaseous Hydrogen Rocket Combustion Serdar Yeralan; Sibtosh Pal; Robert J. Santoro Propellant Atomization and Ignition Phenomena in Liquid Oxygen/Gaseous Hydrogen Rocket Combustors Wolfgang O. H. Mayer; Blazenko Ivancic; Axel Schik; Ulf Hornung Combustion Behavior and Flame Structure of XM46 Liquid Propellant 800 794 788 780 772 762 758 753 1133 1131 1129 1123 1117 1109 1100 Y.-P. Chang; E. Boyer; K. K. Kuo Analysis of In-Flight Behavior of Truncated Plug Nozzles F. Nasuti; M. Onofri Evaporation of Sprays of Liquid Fuels and Liquid Oxidizers in a Shear Layer D. Katoshevski; Y. Tambour Sensitivity of Mixed Subsonic-Supersonic Turbulent Mixing Layers D. Chad Cottrell III; Michael W. Plesniak Computation of Compressible Flows Through a Chemical Laser Device with Crossflow Injection James H. Miller; Joe S. Shang; Robert F. Tomaro; William Z. Strang Convergence Behavior of Surface Evolver Applied to a Generic Propellant-Management Device Steven H. Collicott Combustion of Magnesium with Carbon Dioxide and Carbon Monoxide at Low Gravity Angel Abbud-Madrid; Abhijit Modak; Melvyn C. Branch; John W. Daily Combustion Characteristics of a Liquid-Fueled Ramjet Combustor Takao Inamura; Mamoru Takahashi; Akinaga Kumakawa Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview Adela Ben-Yakar; Ronald K. Hanson Internally Mixed Liquid Injector for Active Control of Atomization Process A. Kushari; Y. Neumeier; O. Israeli; E. Lubarsky; B. T. Zinn Random Packs and Their Use in Modeling Heterogeneous Solid Propellant Combustion S. Kochevets; J. Buckmaster; T. L. Jackson; A. Hegab Blade-Row Interaction in a High-Pressure Turbine V. S. P. Chaluvadi; A. I. Kalfas; M. R. Banieghbal; H. P. Hodson; J. D. Denton Hub Wall Rotation Influence on High-Speed Compressor Cascade Performance A. Doukelis; K. Mathioudakis; K. Papailiou Nonlinear Dynamic Combustion in Solid Rockets: L* Effects K. C. Tang; M. Q. Brewster Actuator Duct Model of Turbomachinery Components for PoweredNacelle Navier-Stokes Calculations Entsung Hsiao; Mahmood Naimi; Jeffrey P. Lewis; Keith Dalbey; Yifang Gong; Choon Tan Aeroacoustic Measurement of Transient Hot Nozzle Flows Daniel R. Kirk; Douglas O. Creviston; Ian A. Waitz Technical Notes 928 919 909 902 892 883 878 869 860 852 845 836 823 818 809 Downstream Gas Effect on Nozzle Flow-Separation Location John W. Murdock; Richard P. Welle Adaptive Analysis of the Inviscid Supersonic Flow over a BackwardFacing Step S. Y. Yang Effect of Reynolds Number on Pitot-Pressure Distributions in Underexpanded Supersonic Freejets Hiroshi Katanoda; Taro Handa; Yoshiaki Miyazato; Mitsuharu Masuda; Kazuyasu Matsuo Numerical Evaluation of Inelastic Mechanisms in a Nitrogen Arcjet Shigeru Kuchi-Ishi; Michio Nishida Volume 17 Number 3 May 2001 Full-Length Papers Laser Doppler Anemometry Measurements in an Axial Compressor Stage Thierry M. Faure; Guy-Jean Michon; Hubert Miton; Nicolas Vassilieff Shape Parameterization and Optimization of a Two-Stroke Engine Angelos P. Mimis; Malcolm I. G. Bloor; Michael J. Wilson Mars-Earth Rapid Interplanetary Tether Transport System: I. Initial Feasibility Analysis Gerald D. Nordley; Robert L. Forward Spectral Content of Solar Radiation on Martian Surface Based on Mars Pathfinder J. Appelbaum; A. Steiner; G. A. Landis; C. R. Baraona; T. Segalov Ion Propulsion Development Projects in U.S.: Space Electric Rocket Test I to Deep Space 1 James S. Sovey; Vincent K. Rawlin; Michael J. Patterson Development and Validation of Fluid/Thermodynamic Models for Spacecraft Propulsion Systems Henry C. Hearn Safe Testing of Nuclear Rockets Steven D. Howe; Bryan Travis; David K. Zerkle Search for Nuclear Isotopes for Use in a Nuclear Battery B. D. Guenther; H. R. Weller; Jennifer L. Godwin Review of Refractory Materials for Alkali Metal Thermal-to-Electric Conversion Cells Jeffrey C. King; Mohamed S. El-Genk Stress and Buckling Analyses of Multitube, Vapor-Anode, Nb-1Zr/C-103 AMTEC Cells Jeffrey C. King; Mohamed S. El-Genk Analysis of Heat-Driven Jet-Pumped Cooling System for Space Thermal Management 936 938 940 943 481 492 499 508 517 527 534 540 547 557 566 J. W. Nord; W. E. Lear; S. A. Sherif Computational Optimization of a Hypersonic Rectangular-to-Circular Inlet John W. Sabean; Mark J. Lewis Sidewall Interaction in an Asymmetric Simulated Scramjet Inlet Configuration D. V. Gaitonde; M. R. Visbal; J. S. Shang; A. A. Zheltovodov; A. I. Maksimov Manipulation of Shock/Boundary-Layer Interactions in Hypersonic Inlets D. Schulte; A. Henckels; R. Neubacher Theoretical Performance of Frictionless Magnetohydrodynamic-Bypass Scramjets Chul Park; David Bogdanoff; Unmeel B. Mehta Propulsive Performance of Hypersonic Oblique Detonation Wave and Shock-Induced Combustion Ramjets J. P. Sislian; H. Schirmer; R. Dudebout; J. Schumacher Effects of Fuel Preinjection on Mixing in Mach 1.6 Airflow Michael Owens; Sudarshan Mullagiri; Corin Segal; Viacheslav A. Vinogradov Thermal Choking Analyses in a Supersonic Combustor M. G. Owens; S. Mullagiri; C. Segal; P. J. Ortwerth; A. B. Mathur Thrust, Lift, and Pitching Moment of a Scramjet Engine Takashi Shimura; Noboru Sakuranaka; Tetsuji Sunami; Kouichiro Tani Small-Bore Ram Accelerator Operation A. Sasoh; Y. Hamate; K. Takayama Aerothermal Model for Real-Time Digital Simulation of a Mixed-Flow Turbofan Engine Vivek Sanghi; B. K. Lakshmanan; R. Rajasekaran Unified Treatment of Flow Instabilities of Turbomachines Yoshinobu Tsujimoto; Kenjiro Kamijo; Christopher E. Brennen Tip Leakage Flow in a Radial Inflow Turbine with Varying Gap Height R. Dambach; H. P. Hodson Analysis of Unsteady Blade Row Interaction Using Nonlinear Harmonic Approach T. Chen; P. Vasanthakumar; L. He Development and Validation of a Massively Parallel Flow Solver for Turbomachinery Flows Jixian Yao; Antony Jameson; Juan J. Alonso; Feng Liu Redesigning Gas-Generator Turbines for Improved Unsteady Aerodynamic Performance Using Neural Networks Nateri K. Madavan; Man Mohan Rai; Frank W. Huber Influence of Compressor Exit Conditions on Combustor Annular Diffusers, Part 1: Diffuser Performance 678 669 659 651 644 636 629 622 617 611 605 599 591 585 579 571 A. G. Barker; J. F. Carrotte Influence of Compressor Exit Conditions on Combustor Annular Diffusers Part II: Flow Redistribution A. G. Barker; J. F. Carrotte Turbojet and Turbofan Engine Performance Increases Through Turbine Burners F. Liu; W. A. Sirignano Pressure Waves in Volume Effect in Gas-Turbine TransientPerformance Models Y. G. Li; N. R. L. MacCallum; P. Pilidis Pressure Drop Across a Double-Outlet Vortex Chamber Georgios H. Vatistas; Peter Sakaris Parametric Study of the Swirler/Venturi Spray Injectors Kyoung-Su Im; Hoisan Kim; Ming-Chia Lai; Robert Tacina On the Breakup of Viscous Liquid Sheets by Dual-Mode Linear Analysis Sushanta K. Mitra; Xianguo Li; Metin Renksizbulut Mixing Mechanisms in a Pair of Impinging Jets Nasser Ashgriz; William Brocklehurst; Douglas Talley Technical Note Studies on Performance of Airblast Atomizer Under Varying Flow and Geometric Conditions S. N. Sridhara; B. N. Raghunandan Volume 17 Number 2 March 2001 Full-Length Papers Gear Fault Detection in Rocket Engine Turbomachinery S. J. Dimaggio; S. Rubin; B. H. Sako Oscillating Airfoil Aerodynamics of a Rotating Compressor Blade Row Kuk Kim Frey; Sanford Fleeter 240 Michael K. Fabian; Eric A. Falk; Eric J. Jumper Control of Blade Flutter by Smart-Casing Treatment Xiaofeng Sun; Xiaodong Jing; Hongwu Zhao Comparison of Methods for Calculating Turbine Work in the Air Turborocket K. L. Christensen Upstream-Propagating Potential Disturbances in the F109 Turbofan Engine Inlet Flow Eric A. Falk; Eric J. Jumper; Michael K. Fabian; Jerry Stermer Analysis of a Device for Generating Perturbations in Supersonic Wind Tunnels 270 262 256 248 232 225 750 736 728 717 711 706 695 687 Kevin J. Melcher; Mounir B. Ibrahim Experimental Testing of a Hypersonic Inlet with Rectangular-to-Elliptical Shape Transition M. K. Smart Mole-Fraction-Sensitive Imaging of Hypermixing Shear Layers J. S. Fox; A. F. P. Houwing; P. M. Danehy; M. J. Gaston; N. R. Mudford; S. L. Gai Combustion Tests of a Staged Supersonic Combustor with a Strut Sadatake Tomioka; Atsuo Murakami; Kenji Kudo; Tohru Mitani Combustion Efficiencies of Supersonic Flames Albert Ratner; James F. Driscoll; Hwanil Huh; Rodney A. Bryant Reaction and Mixing-Controlled Combustion in Scramjet Engines Tohru Mitani; Nobuo Chinzei; Takeshi Kanda Scramjet Fuels Autoignition Study Meredith B. Colket III; Louis J. Spadaccini Comparison of Thermodynamic Loss Models Suitable for Gas Turbine Propulsion Bryce A. Roth; Dimitri N. Mavris SCCREAM: A Conceptual Rocket-Based Combined-Cycle Engine Performance Analysis Tool John R. Olds; John E. Bradford High-Energy-Utilization, Dual-Mode System Concept for Mars Missions Mohamed S. El-Genk Structural Dynamic Analysis of Solid Rocket Motor Resonant Burning K. W. Dotson; J. M. Womack; P. J. Grosserode Vorticity Dynamics in Isobarically Closed Porous Channels Part I: Standard Perturbations J. Majdalani Vorticity Dynamics in Isobarically Closed Porous Channels Part II: Space-Reductive Perturbations J. Majdalani; T. S. Roh Periodic Propellant Flames and Fluid-Mechanical Effects T. L. Jackson; J. Buckmaster; A. Hegab Study of a New Kind of Multipulse Rocket Motor Mingde Song; Dingyou Ye Numerical Modeling of Pressurization of a Propellant Tank Alok Majumdar; Todd Steadman Response Surface and Neural Network Techniques for Rocket Engine Injector Optimization Wei Shyy; P. Kevin Tucker; Rajkumar Vaidyanathan Mixing Characteristics of Coaxial Injectors at High Gas/Liquid Momentum Ratios 402 391 385 380 371 363 355 347 340 333 324 315 308 301 293 284 276 P. A. Strakey; D. G. Talley; J. J. Hutt Advanced Sub-Model for Airblast Atomizers Y. Liao; S. M. Jeng; M. A. Jog; M. A. Benjamin Near-Field Ion Energy and Species Measurements of a 5-kW Hall Thruster Frank S. Gulczinski III; Alec D. Gallimore Internal Plasma Properties and Enhanced Performance of 8-Centimeter Ion Thruster Discharge John E. Foster; Michael J. Patterson Plasma Confinement in the Whistler Wave Plasma Thruster B. W. Stallard; E. B. Hooper Jr; J. L. Power Thermal Decomposition of RDX in the Presence of Added K2B12H12 Michael A. Schroeder; Robert A. Fifer; Pamela J. Kaste; Shirley A. Liebman Direct Evidence of Spatial Burning Rate Variation as Cause of Midweb Anomaly Desh Deepak; R. Jeenu; P. Sridharan; M. S. Padmanabhan Combustion of Kerosene in Counterflow Diffusion Flames P. M. Patterson; A. G. Kyne; M. Pourkashanian; A. Williams; C. W. Wilson Surrogate Mixtures to Represent Complex Aviation and Rocket Fuels Tim Edwards; Lourdes Q. Maurice Analysis and Design of the Inductor-Current-Sensing Peak-PowerTracking Solar-Array Regulator Yoon-Jay Cho; Bo-Hyung Cho Technical Notes Optimal Geometry of Self-Field Magnetoplasmadynamic Thrusters Guido Colasurdo; Lorenzo Casalino Transonic Compressor Influences on Upstream Surface Pressures with Axial Spacing Peter J. Koch; Douglas P. Probasco; J. Mitch Wolff; William W. Copenhaver; Randall M. Chriss Thermodynamic Cycle Analysis of Magnetohydrodynamic-Bypass Hypersonic Airbreathing Engines Ron J. Litchford; John W. Cole; Valentine A. Bityurin; John T. Lineberry Volume 17 Number 1 January 2001 Editorial A Distinguished Career. . .and a New Beginning Roger L. Simpson To Everything There Is a Season R. H. Woodward Waesche 2 1 477 474 472 467 461 453 449 441 433 428 418 411 Thank You and Best Wishes to Dr. R. H. Woodward Waesche Vigor Yang Reviewers for October 1999-September 2000 Editorial Policy Statement on Numerical Accuracy and Experimental Uncertainty Ethical Standards for Publication of Aeronautics and Astronautics Research AIAA Manuscript Review Process Full-Length Papers Erosion Resistance of Carbon-Carbon Ion Optics J. S. Meserole Magnetohydrodynamics Generator with Plasma Layers as Power Source Aboard a Hypersonic Airplane Vadim S. Slavin; Valery M. Gavrilov; Nikolay I. Zelinsky; Alexandr R. Bozhkov Development of Ultraviolet Raman Diagnostics for Rocket Engine Injector Analysis Joseph A. Wehrmeyer; John M. Cramer; Richard H. Eskridge; Chris C. Dobson Fuel Regression Rate in Hydroxyl-Terminated-Polybutadiene/GaseousOxygen Hybrid Rocket Motors Philmon George; S. Krishnan; P. M. Varkey; M. Ravindran; Lalitha Ramachandran Upstream Wake Influences on the Measured Performance of a Transonic Compressor Stage Steven E. Gorrell; William W. Copenhaver; Randall M. Chriss Flow and Acoustic Properties of Underexpanded Elliptic-Slot Jets S. B. Verma; E. Rathakrishnan Studies on Combustion of Metallized RDX-Based Composite Modified Double-Base Propellants C. N. Divekar; S. N. Asthana; Haridwar Singh Transient Force Reduction in Electromechanical Actuators for ThrustVector Control Dale E. Schinstock; Douglas A. Scott; Tim A. Haskew Flame Spread with Sudden Expansions of Ports of Solid Propellant Rockets B. N. Raghunandan; V. R. Sanal Kumar; C. Unnikrishnan; C. Sanjeev Scalar Variance Transport in the Turbulence Modeling of Propulsive Jets N. Chidambaram; S. M. Dash; D. C. Kenzakowski Optimization for Aircraft Engines with Regression and Neural-Network Analysis Approximators Surya N. Patnaik; James D. Guptill; Dale A. Hopkins; Thomas M. Lavelle Multidisciplinary Approach to Linear Aerospike Nozzle Design 3 8 9 10 11 12 19 27 35 43 49 58 65 73 79 85 93 J. J. Korte; A. O. Salas; H. J. Dunn; N. M. Alexandrov; W. W. Follett; G. E. Orient; A. H. Hadid Regression-Rate and Heat-Transfer Correlations for Hybrid Rocket Combustion Martin J. Chiaverini; Kenneth K. Kuo; Arie Peretz; George C. Harting Computational Assessment of Afterburning Cessation Mechanisms in Fuel-Rich Rocket Exhaust Plumes William H. Calhoon Jr Gun Interior Ballistic Performance with Ammonium Nitrate-Alcohol Propellants Akihiro Sasoh; Toshihiro Ogawa; Kazuyoshi Takayama; Kazunari Ikuta; Nobuo Nagayasu; Shinobu Ohtsubo Model of Particulate Interaction with Plasma in a Teflon Pulsed Plasma Thruster Michael Keidar; Iain D. Boyd; Isak I. Beilis Mach 8 Testing of a Scramjet Engine Model Takeshi Kanda; Tetsuji Sunami; Sadatake Tomioka; Kouichiro Tani; Tohru Mitani Effect of Sides-Spillage from Airframe on Scramjet Engine Performance Kouichiro Tani; Takeshi Kanda; Kenji Kudo; Daisuke Akihisa Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors M. R. Gruber; R. A. Baurle; T. Mathur; K.-Y. Hsu Effect of Reynolds Number on Separation Bubbles on Compressor Blades in Cascade Garth V. Hobson; Denis J. Hansen; David G. Schnorenberg; Darren V. Grove Amine Sensitization Studies of Secondary Explosives Using LaserInduced Ignition A. L. Ramaswamy; T. Mukundan; M. M. Chaudhri Effects of Interjet Spacing on Burning Multiple Sprays K. Parvez; S. R. Gollahalli Application of Artificial Neural Networks to the Design of Turbomachinery Airfoils Man Mohan Rai; Nateri K. Madavan Novel Electroexplosive Device Incorporating a Reactive Laminated Metallic Bridge Thomas A. Baginski; Steven L. Taliaferro; Wm. David Fahey Pressure Effects on Geometry and Structure of Gas Jet Flames in Crossflow Ahsan R. Choudhuri; S. R. Gollahalli Velocity and Temperature Statistics in Reacting Droplet-Laden Homogeneous Shear Turbulence Farzad Mashayek Origins of Accelerator Grid Current: Analysis of T5 Grid Test Results 203 197 190 184 176 169 163 154 146 139 132 125 120 111 99 Mark W. Crofton; Iain D. Boyd Technical Notes Fluid Property Effects on Sheet Disintegration of a Simplex PressureSwirl Atomizer I-Ping Chung; Cary Presser Characteristic Gap: A New Design Criterion for Solid Rocket Motors Daniel Chasman Concentration Measurements in a Mixing Module for Lean, Premixed, Gas-Turbine Combustors R. V. Ravikrishna; D. Douglas Thomsen; Clayton S. Cooper; Yanan Jiang; Normand M. Laurendeau Radiation and NOx Pathways in Nonpremixed Turbulent Flames D. Lentini; I. K. Puri Volume 16 Number 6 November 2000 Full-Length Papers Optimization of Orifice Geometry for Crossflow Mixing in a Cylindrical Duct J. T. Kroll; W. A. Sowa; G. S. Samuelsen; J. D. Holdeman Comparison of Spray/Wall Impingement Models with Experimental Data Seong Hyuk Lee; Hong Sun Ryou Numerical Study of Fuel Mixing Enhancement Using an Oblique Shock/Vortex Interaction Ashish Nedungadi; Mark J. Lewis Maximum Mixing Times of Methane and Air Dan Brasoveanu; Ashwani K. Gupta Multicomponent-Fuel Film-Vaporization Model for Multidimensional Computations Yangbing Zeng; Chia-Fon Lee Soot Patterns Around Suspended n-Heptane Droplet Flames in a Convection-Free Environment C. Thomas Avedisian; Gregory S. Jackson Effect of Sauter Mean Diameter on the Combustion Related Parameters in Heavy-Duty Diesel Engines Stanislav N. Danov; Ashwani K. Gupta Predicting Effectiveness of H2O Injection for NOx Reduction in Stationary Gas Turbines A. M. Mellor Broadband Infrared Absorption Sensor for High-Pressure Combustor Control J. M. Seitzman; B. T. Scully Computation of Gas-Liquid Droplet Cascade Flows Using Multigrid Adaptive Unstructured Grid 1002 994 988 980 974 964 956 946 939 929 222 218 216 212 Ki-Cheol Park; Keun-Shik Chang Performance of Evaporative Cycle Gas Turbines Derived from Aeroengines Sergio Mario Camporeale; Bernardo Fortunato Determination of Triggering Condition of Vortex-Driven Acoustic Combustion Instability in Rocket Motors Wen-Jing Wu; Li-Chung Kung Computational Analysis for Rocket-Based Combined-Cycle Systems During Rocket-Only Operation C. J. Steffen Jr; T. D. Smith; S. Yungster; D. J. Keller Starting Envelope of the Subdetonative Ram Accelerator E. Schultz; C. Knowlen; A. P. Bruckner Work Interaction in Quasi-One-Dimensional Flows Thomas Scott; David W. Riggins Longitudinally Stratified Combustion in Wave Rotors M. Razi Nalim Solid-Fuel Ramjet Regulation by Means of an Air-Division Valve Deborah Pelosi-Pinhas; Alon Gany Impingement Heating and Ignition of Condensed-Phase Energetic Materials Mohammad K. Alkam; P. Barry Butler Development of the Low-Power Xenon Ion Thruster for Lightweight Satellites O. A. Gorshkov; V. G. Grigor'yan; V. A. Muravlev Mass Spectral Measurements in the Plume of an SPT-100 Hall Thruster Lyon B. King; Alec D. Gallimore Electrical Characteristics of Magnetohydrodynamic-Generator Sidewalls with Segmented Z-Bar Design Carlson C. P. Pian; Stanley W. Petty Pulsed Fusion Propulsion System for Rapid Interstellar Missions Terry Kammash Regenerative Solid Oxide Fuel Cells for Mars Exploration K. R. Sridhar; R. Foerstner Optimal Allocation with Network Limitation for Autonomous Space Power System James A. Momoh; Jizhong Zhu; Jim L. Dolce Application of Bethe-Zel'dovich-Thompson Fluids in Organic Rankine Cycle Engines Brady P. Brown; Brian M. Argrow Performance Analysis for High-Speed Missile Inlets Christophe Bourdeau; Michaël Blaize; Doyle Knight 1125 1118 1112 1105 1100 1093 1086 1083 1075 1069 1060 1053 1040 1030 1022 1011 Automated Design of a Three-Dimensional Subsonic Diffuser Wei-Li Zhang; Doyle D. Knight; Don Smith Simulation of Coupled Unsteady Flow and Heat Conduction in Turbine Stage Douglas L. Sondak; Daniel J. Dorney Mechanical Coupling Effects on Turbomachine Mistuned Response James A. Kenyon; Charles J. Cross; Gregory R. Minkiewicz Hub-Based Vibration Control of Multiple Rotating Airfoils György Szász; George T. Flowers; Roy J. Hartfield Linear Versus Quadratic Amplitude Feedback in Active Control of Compressor Rotating Stall Nikos Markopoulos; Yedidia Neumeier; J. V. R. Prasad; Ben T. Zinn Three-Dimensional Automatic Optimization Method for Turbomachinery Blade Design K. F. C. Yiu; M. Zangeneh Technical Note Thixotropic Effect of Inorganic Gel Fuels Shai Rahimi; Benveniste Natan Volume 16 Number 5 September 2000 Full-Length Papers Optimization of Jet Mixing into a Rich, Reacting Crossflow M. Y. Leong; G. S. Samuelsen; J. D. Holdeman Propagation of Spinning Acoustic Modes in Turbofan Exhaust Ducts M. Nallasamy; D. L. Sutliff; L. J. Heidelberg Unsteady Viscous Flow Causing Rotor-Stator Interaction in Turbines, Part 1: Data, Code Pressure B. Lakshminarayana; A. Chernobrovkin; D. Ristic Unsteady Viscous Flow Causing Rotor-Stator Interaction in Turbines, Part 2: Simulation, Integrated Flowfield, and Interpretation A. Chernobrovkin; B. Lakshminarayana Analytical and Experimental Assessment of Two Methods of Determining Turbine Efficiency Susan T. Hudson; Hugh W. Coleman Unsteady Blade-Row Flow Calculations Using a Low-Reynolds-Number Turbulence Model Chang Ho Choi; Jung Yul Yoo Fluid Circuit Model for Long-Bearing Squeeze Film Damper Rotordynamics Paul A. Schallhorn; David A. Elrod; David G. Goggin; Alok K. Majumdar Bleed Valve Rate Requirements Evaluation in Rotating Stall Control on Axial Compressors 1132 1141 1149 1155 1164 1174 1182 729 736 744 751 760 768 777 781 Simon Yeung; Yong Wang; Richard M. Murray Dynamic Simulation of a Wave-Rotor-Topped Turboshaft Engine R. B. Greendyke; D. E. Paxson; M. T. Schobeiri Survey of Advancements in Jet-Engine Thermodynamic Simulation Vivek Sanghi; B. K. Lakshmanan; V. Sundararajan Analysis of Transient Thermal Choking Processes in a Model Scramjet Engine S. O'Byrne; M. Doolan; S. R. Olsen; A. F. P. Houwing Design and Control of Solid-Fuel Ramjet for Pseudovacuum Trajectories S. Krishnan; Philmon George; S. Sathyan Injection and Mixing Processes in High-Pressure Liquid Oxygen/Gaseous Hydrogen Rocket Combustors W. Mayer; A. Schik; M. Schäffler; H. Tamura Analysis of Gaseous Fuel and Air Mixing in Flames and Flame Quenching Dan Brasoveanu; Ashwani K. Gupta Effect of Inlet Turbulence and Premixer Length on Fuel Distribution in Swirling Gas-Turbine Premixer S. F. Frey; A. R. Eaton; D. M. Cusano; M. W. Plesniak; P. E. Sojka Role of Oxygen-Enriched Atomization in Kerosene Spray Flames A. K. Gupta; T. Damm; S. R. Charagundla; C. Presser Overview of World Space Launches I-Shih Chang Oscillatory Combustion of Fine-AP/HTPB Propellants: Disproportionate Pyrolysis Response S. R. Hickman; M. Q. Brewster Prediction of the Dissipation of a Solid-Rocket Contrail Eugene Miller On-Orbit Demonstration of a Pulsed Self-Field Magnetoplasmadynamic Thruster System K. Toki; Y. Shimizu; K. Kuriki Applied-Field Magnetoplasmadynamic Thrusters, Part 1: Numerical Simulations Using the MACH2 Code Pavlos G. Mikellides; Peter J. Turchi; Norman F. Roderick Applied-Field Magnetoplasmadynamic Thrusters, Part 2: Analytic Expressions for Thrust and Voltage Pavlos G. Mikellides; Peter J. Turchi Computation of the Plume of an Anode-Layer Hall Thruster Iain D. Boyd Investigation of the Operating Characteristics of a High-Power Hall Effect Thruster Boris Arhipov; Leonid Krochak; Nikolay Maslennikov; Fabrizio Scortecci 910 902 894 887 880 874 867 853 845 837 829 823 815 808 797 792 Ion-Energy Diagnostics in the Plasma Exhaust Plume of a Hall Thruster Lyon B. King; Alec D. Gallimore Antimatter Requirements and Energy Costs for Near-Term Propulsion Applications G. R. Schmidt; H. P. Gerrish; J. J. Martin; G. A. Smith; K. J. Meyer Volume 16 Number 4 July 2000 Editorial Norio Arai; Kuni Kitagawa; Ashwani K. Gupta Advanced Terrestrial Energy Conversion Advanced Power Generation R. H. Woodward Waesche Utilization of High-Density Strained Hydrocarbon Fuels for Propulsion Gabriel D. Roy Analysis of Combustion Characteristics of Coaxial Jet Diffusion Flame with Steam Addition D. Zhao; H. Yamashita; T. Furuhata; N. Arai Power Generation Analysis for High-Temperature Gas Turbine in Thermodynamic Process Hiroshi Taniguchi; Sigehiro Miyamae; Norio Arai; Noam Lior Double Reheat Rankine Cycle for Hydrogen-Combustion, Turbine Power Plants Masafumi Fukuda; Yoshikazu Dozono Enhancing Direct-Fired Power Plants Performance by Use of Gas Turbine Technology Mikhail Korobitsyn Status and Perspective of Externally Fired Gas Turbines J. Yan; L. Eidensten Miniaturization Technologies for Advanced Energy Conversion and Transfer Systems Timothy A. Ameel; Ian Papautsky; Robert O. Warrington; Robert S. Wegeng; M. Kevin Drost Gas Turbine Heat Transfer: Past and Future Challenges Ralf Schiele; Sigmar Wittig Investigation of Regenerative Combustion Using a Heavy Fuel Oil I-Te Huang; Wen-Chen Chang; Wei-Min Chern; Rey-Chein Chang Visualization of Fuel Jet in Conditions of Highly Preheated Air Combustion S. Lille; T. Dobski; W. Blasiak Characteristics of Pulverized Coal Combustion in High-Temperature Preheated Air Takashi Kiga; Kunio Yoshikawa; Masaru Sakai; Susumu Mochida 916 923 545 545 546 552 557 562 568 572 577 583 590 595 601 Gasification Characteristics of Biomass Wastes in Fluidized Bed Gasifier Ping Liu; Xiaofen Guo; Chuangzhi Wu; Yong Chen; Norio Arai Modeling of Oxy-Natural Gas Combustion Chemistry Anders Brink; Mikko Hupa; Frederic Breussin; Nicolas Lallemant; Roman Weber Thermal Destruction of Cellulose and Surrogate Solid Wastes Ashwani K. Gupta Stability of Plane Liquid Sheets in Compressible Gas Streams Jianming Cao; Xianguo Li Recent Advances in Soot Formation from Spherical Droplet Flames at Atmospheric Pressure C. Thomas Avedisian Influence of Exhaust Aftertreatment Devices on Heavy-Duty Diesel Engine's Particulate Emissions George Toussimis; Euripides Lois; Hartmut Lüders Fire Development Calculations David G. Lilley Minimum Safe Distance from Pool Fires David G. Lilley Transition in Boundary Layers on a Concave Surface S. H. Winoto; D. H. Zhang; Y. T. Chew Full-Length Papers Localized Thermal Buckling Due to Hot Streaks in a Combustor Liner W. Z. Zhuang; N. S. Swansson Thermal State-of-Charge of Space Solar Dynamic Heat Receivers Carsie A. Hall III; Emmanuel K. Glakpe; Joseph N. Cannon; Thomas W. Kerslake Effect of Initial Velocity Profile on the Development of Round Jets E. Ferdman; M. V. Ötügen; S. Kim Feasibility Study for Performance Prediction of Circumferentially Compound-Stage Model Turbines André P. Saxer; Hélène M. Saxer-Felici; Damian M. A. Vogt; Michael Sell; George Gyarmathy Numerical Investigation of Installation Effects in Turbofan Engines W. G. Joo Energy Management in Rocket Propulsion Guido Colasurdo; Lorenzo Casalino Comparison of Supersonic Combustion Between Impulse and VitiationHeated Facilities R. R. Boyce; A. Paull; R. J. Stalker; M. Wendt; N. Chinzei; H. Miyajima Technical Notes 606 609 615 623 628 636 641 649 653 661 666 676 687 697 705 709 Unstarted Inlet for Direct-Connect Combustor Experiments in a Shock Tunnel R. R. Boyce; A. Paull; R. J. Stalker Reference Spray Combustion Facility for Computational Fluid Dynamics Model Validation John F. Widmann; S. Rao Charagundla; Cary Presser Role of Curing Agents on Decomposition and Explosion of Glycidyl Azide Polymers Surendra P. Panda; Sanjay K. Sahu; Dinkar S. Sadafule; Jyotsna V. Thakur Numerical Simulation of Axisymmetric Solid Rocket Motor Ignition Transient with Radiation Effect In Hyun Cho; Seung Wook Baek Volume 16 Number 3 May 2000 Full-Length Papers Effects of Radial Location on the Migration of Hot Streaks in a Turbine Karen L. Gundy-Burlet; Daniel J. Dorney Viscous Three-Dimensional Simulation of Transonic Compressor Stage on Parallel Hardware Gerd Fritsch; Martin Hoeger; Cristoph Blaha; Dirk Bauer Incidence Effects on Wake-Induced Transition on an Axial Compressor Blade W. J. Solomon; G. J. Walker Experiment to Support the Formulation and Validation of CompressorFace Boundary Conditions Donald Freund; Miklos Sajben Adiabatic Interaction of Particles with a Compressible Flow: Basic Mechanics Francisco Ruiz Experimental Investigation of Rotor-Inlet Guide Vane Interactions in Transonic Axial-Flow Compressor Albert J. Sanders; Sanford Fleeter Evaluating Efficiencies of Turbofan Jet Engines: A Data Envelopment Analysis Approach Sean Bulla; William W. Cooper; Dennis Wilson; Kyung Sam Park Scarfing and Scalloping Effects on Lobed Forced Mixer at Low-Speed Conditions S. C. M. Yu; Y. Hou; W. K. Chan Transverse Injection from Circular and Elliptic Nozzles into a Supersonic Crossflow M. R. Gruber; A. S. Nejad; T. H. Chen; J. C. Dutton Flow of Gel Fuels in Tapered Injectors Shai Rahimi; Benveniste Natan 718 720 723 725 377 388 397 406 415 421 431 440 449 458 Streamline Tracing: Technique for Designing Hypersonic Vehicles Frederick S. Billig; Ajay P. Kothari Wall Drag in Internal Mach-2 Flow with Cavity and Transpiration Injection Linda A. Castiglone; G. Burton Northam; Ned R. Baker; Larry A. Roe Restricted Shock Separation in Rocket Nozzles Manuel Frey; Gerald Hagemann Combustor Model for Simulation of Combustion Instabilities and Their Active Control Rajendran Mohanraj; Yedidia Neumeier; Ben T. Zinn Convergence of Two Analytical Flowfield Models Predicting a Destabilizing Agent in Rocket Combustion J. Majdalani; G. A. Flandro; T. S. Roh Nonpremixed Periodic Flames Supported by Heterogeneous Propellants T. L. Jackson; J. Buckmaster Line-of-Sight Variations of Temperature and Species in Solid Propellant Flames Carl F. Mallery Jr.; Stefan T. Thynell Flame/Stretch Interactions of Premixed Fuel-Vapor/O2/N2 Flames O. C. Kwon; M. I. Hassan; G. M. Faeth Ultrasonic Method Applied to Full-Scale Solid Rocket Motors Franck Cauty Measurements of Ions from High-Current Hollow Cathodes Using Electrostatic Energy Analyzer Ikuya Kameyama; Paul J. Wilbur Three-Dimensional Numerical Simulation of Field-Emission-ElectricPropulsion Neutralization M. Tajmar; J. Wang Volume 16 Number 2 March 2000 Full-Length Papers Confined Swirling Flows with Heat Release and Mixing David S. Underwood; Ian A. Waitz; Edward M. Greitzer Numerical Investigation of Twin-Nozzle Rocket Plume Phenomenology Houshang B. Ebrahimi; Jay Levine; Alan Kawasaki Detailed Chemical-Kinetic Model for Aviation Fuels R. P. Lindstedt; L. Q. Maurice Thrust Vector Control for (Clustered Modules) Plug Nozzles: Some Considerations H. F. R. Schöyer Optimizing Subcritical-Flow Thrust-Vectoring of Converging-Diverging Nozzles 465 472 478 485 492 498 505 513 523 529 536 169 178 187 196 202 Nozzles Erich A. Wilson; Dan Adler; Benjamin Z. Bal-Or; Valery Sherbaum; Michael Lichtsinder Direct Computation of Jet Noise Produced by Large-Scale Axisymmetric Structures R. R. Mankbadi; H. Shih; R. Hixon; L. A. Povinelli Flowfield near a Mulitiport Injector Array in a Supersonic Flow L. S. Jacobsen; J. A. Schetz; W. F. Ng Ignition Characteristics of Plasma Torch for Hydrogen Jet in an Airstream Kenichi Takita; Tomokazu Uemoto; Takahiro Sato; Yiguang Ju; Goro Masuya; Katsura Ohwaki Two-Dimensional Nonadiabatic Injection into a Supersonic Freestream Rodney D. W. Bowersox; K. Colin Tucker; Christopher D. Whitcomb Propulsion System for Hypersonic Space Planes Michael Zeutzius; Toshiaki Setoguchi; Kunio Terao; Hideo Miyanishi Pulse Detonation Magnetohydrodynamic Power Ron J. Litchford; Bryan R. Thompson; John T. Lineberry Magnetocombustion: A Thermodynamic Analysis John Baker; Kozo Saito Optimization of Ram Accelerator Systems Design Xiaojian Wang; Elyeser Spiegler; Yaakov M. Timnat Experimental Investigation of the Evaporation of Droplets in Axial Acoustic Fields R. I. Sujith; G. A. Waldherr; J. I. Jagoda; B. T. Zinn Effect of Inlet Conditions on Endwall Secondary Flows Kristina S. Hermanson; Karen A. Thole Effect of Inner and Outer Airflow Characteristics on High Liquid Pressure Prefilming Airblast Atomization J. S. Chin; N. K. Rizk; M. K. Razdan Progress in Modeling Pressure Oscillations in Regenerative Liquid Propellant Guns T. P. Coffee Eulerian Approach for Unsteady Two-Phase Solid Rocket Flows with Aluminum Particles Eric Daniel Combustion Experiments in Hydrogen Peroxide/Polyethylene Hybrid Rocket with Catalytic Ignition E. J. Wernimont; S. D. Heister Time-Accurate Three-Dimensional Navier-Stokes Analysis of One-andOne-Half Stage Axial-Flow Turbine Thomas W. Volmar; Bernard Brouillet; Heinz E. Gallus; Hannes Benetschik 327 318 309 302 297 286 278 269 263 251 243 234 227 216 207 Modeling of Turbine Engine Axial-Flow Compressor and Turbine Characteristics Marek Orkisz; Slawomir Stawarz New Gear-Fault-Detection Parameter by Use of Joint Time-Frequency Distribution V. V. Polyshchuk; F. K. Choy; M. J. Braun Feasibility Assessment of Thermal Barriers for Extreme Transient Temperatures Bruce M. Steinetz; Patrick H. Dunlap Jr Numerical Thermal Model of NASA Solar Electric Propulsion Technology Application Readiness Ion Thruster Jonathan Van Noord; Alec Gallimore; Vincent K. Rawlin Technical Notes Joint Jet-A/Silane/Hydrogen Reaction Mechanism Mark J. Lewis; Jee Su Chang Lithium Peroxide Fuel Cells for Electric Vehicle Propulsion Gautum Agarwal Simulations of the Flow in Supersonic Turbines with Straight Centerline Nozzles Daniel J. Dorney; Lisa W. Griffin; Karen L. Gundy-Burlet Burning Behavior of Composite Propellants with Fast-Burning Inclusions A. E. Fogelzang; A. P. Denisyuk; V. V. Serushkin; V. Yu. Egorshev; V. P. Sinditskii; A. D. Margolin Volume 16 Number 1 January 2000 Editorial Forward into the New Millennium R. H. Woodward Waesche Reviewers for October 1998-September 1999 Editorial Policy Statement on Numerical Accuracy and Experimental Uncertainty Ethical Standards for Publication of Aeronautics and Astronautics Research AIAA Manuscript Review Process Full-Length Papers Aerodynamic Analysis of an Installed Thrust Reverser Daniel J. Strash; J. Michael Summa; Joel H. Frank; Robert Standish Numerical Simulations and Planar Laser-Induced Fluorescence Imaging Results of Hypersonic Reactive Flows Kazu Toshimitsu; Akiko Matsuo; Michel R. Kamel; Christopher I. Morris; Ronald K. Hanson Numerical Investigation of Hydrogen Strut Injections into Supersonic Airflows 336 340 347 357 365 367 370 374 1 6 7 8 9 10 16 22 P. Gerlinger; D. Brüggemann Fuel Injection into a Supersonic Airflow by Means of Pylons C. Gruenig; V. Avrashkov; F. Mayinger Self-Ignition and Supersonic Reaction of Pylon-Injected Hydrogen Fuel C. Gruenig; V. Avrashkov; F. Mayinger Incomplete Mixing and Off-Design Effects on Shock-Induced Combustion Ramjet Performance J. P. Sislian; R. Dudebout; J. Schumacher; M. Islam; T. Redford Three-Dimensional Flow Analysis of Turbine Blade Cascades with Leading-Edge Ejection Dieter Bohn; Volker Becker; Karsten Kusterer; Leonhard Fottner; Sabine Ardey Trailing-Edge Blowing for Reduction of Turbomachinery Fan Noise J. M. Brookfield; I. A. Waitz Computational Analysis of Stall and Separation Control in Centrifugal Compressors Alex Stein; Saeid Niazi; L. N. Sankar Evaluation of Boundary Conditions for the Gust-Cascade Problem R. Hixon; S.-H. Shih; R. R. Mankbadi Identifying Optimal Fan Compressor Pressure Ratios for the MixedStream Turbofan Engine Paul T. Millhouse; Stuart C. Kramer; Paul I. King; Edward F. Mykytka Engine Case Externals Challenges and Opportunities Mike Miller; Jeff Colehour; Ken Dunkelberg Very-Near-Field Plume Investigation of the Anode Layer Thruster Matthew T. Domonkos; Alec D. Gallimore; Colleen M. Marrese; James M. Haas Third Way of Development of Single-Stage-to-Orbit Propulsion V. V. Balepin; M. Maita; S. N. B. Murthy Ideal Gas Thermodynamic Properties of Propellants and Explosive Compounds Alexander Burcat Mass Production of Antimatter for High-Energy Propulsion Brice N. Cassenti Regression Rate Behavior of Hybrid Rocket Solid Fuels Martin J. Chiaverini; Nadir Serin; David K. Johnson; Yeu-Cherng Lu; Kenneth K. Kuo; Grant A. Risha Phase-Stabilized Ammonium Nitrate-Based Propellants Using Binders with N-N Bonds Charlie Oommen; Sampat R. Jain Improvements in the Chemical Stability of Double-Base Solid Rocket Propellants M. H. Sammour 139 133 125 119 105 99 91 87 79 72 65 57 49 41 35 29 Technical Notes Wall Curvature Effects on External Burning in Supersonic Flow Giuseppe Bussi; Dario Pastrone; Lorenzo Casalino Three-Dimensional Disturbance Vortex Method for Simulating Rotor/Stator Interaction in Turbomachinery Xian Hong Wu; Mao Zhang Chen Measurements of Turbulent Flow Structure in Supersonic Curved Wall Boundary Layers R. D. W. Bowersox; R. C. Wier; D. D. Glawe; S. Gogineni Trajectory of a Liquid Jet Traversing Subsonic Airstreams Takao Inamura Preliminary Mass Spectrometry of a Xenon Hollow Cathode Mark W. Crofton Study of Boundary-Layer Development in a Two-Stage Low-Pressure Turbine Daniel J. Dorney; David E. Ashpis; David E. Halstead; David C. Wisler Technical Comments Comment on “Triggering of Longitudinal Combustion Instabilities in Rocket Motors: Nonlinear Combustion Response” V. S. Burnley; F. E. C. Culick Reply by the Authors to V. S. Burnley and F. E. C. Culick J. M. Wicker; V. Yang Comment on “Shock-Loss Model for Transonic and Supersonic Axial Compressors with Curved Blades” N. A. Cumpsty; C. Freeman Reply by the Author to N. A. Cumpsty and C. Freeman M.T. Schobeiri Volume 15 Number 5 September 1999 Full-Length Papers Mixing of Jet Air with a Fuel-Rich, Reacting Crossflow M. Y. Leong; G. S. Samuelsen; J. D. Holdeman Aerodynamic Synthesis of a Centrifugal Impeller Using Computational Fluid Dynamics and Measurements L. M. Larosiliere; G. J. Skoch Surface Pressure Measurements in Supersonic Transverse Injection Flowfields M. R. Gruber; L. P. Goss Expansion and Mixing Processes of Underexpanded Supercritical Fuel Jets Injected into Superheated Conditions Pei-Kuan Wu; Mehrdad Shahnam; Kevin A. Kirkendall; Campbell D. Carter; Abdollah S. Nejad 642 633 623 617 168 166 165 164 160 157 155 153 150 147 Vane Row Indexing for Passive Vibration Control of Axial-Flow Turbomachine Rotors Albert J. Sanders; Sanford Fleeter Probabilistic Analysis of Aircraft Gas Turbine Disk Life and Reliability Matthew E. Melis; Erwin V. Zaretsky; Richard August Effect of Variable Axial Chord on a Low-Pressure Turbine Blade C. G. Murawski; K. Vafai Aerodynamic Effects on Blade Vibratory Stress Variations James A. Kenyon; Douglas C. Rabe; Sanford Fleeter Individual Cylinder Model of a General Aviation Aircraft Engine Gary Parker; Giorgio Rizzoni Apparent Failure of Scaling Methods in Ramjet Connected-Pipe Testing John A. Blevins; Hugh W. Coleman Shock-Tunnel Skin-Friction Measurement C. P. Goyne; R. J. Stalker; A. Paull Air Turborocket/Vehicle Performance Comparison Kirk Christensen Industrial Constraints for Developing Solid Propellants with Energetic Materials Bruno D'Andrea; Francesca Lillo Methodology for Analysis of Postshock Oscillations During PulseTriggered Instability P. G. Harris; A. De Champlain Technical Notes Volume 15 Number 4 July 2001 Full-Length Papers Interferometric Study of Unsteady Passing Shock Flow in a Turbine Cascade A. Wesner; J. A. Schetz; H. Grabowski Fixed-Pitch Propeller/Piston Aircraft Operations at Partial Throttle John T. Lowry Review of Computational Aeroacoustics in Propulsion Systems R. R. Mankbadi Numerical Study of Cavitation in the Wake of a Hypervelocity Underwater Projectile Richard Saurel; Pierre Cocchi; P. Barry Butler Influence of Turbulence Modeling on the Performance Prediction for Rocket Engine Nozzles Frank A. Haidinger Hybrid Monte Carlo-Particle-in-Cell Simulation of an Ion Thruster Plume 650 658 667 675 681 689 699 706 713 719 729 489 497 504 513 523 530 Douglas B. Vangilder; Gabriel I. Font; Iain D. Boyd Simulation of Unsteady Flow in Nozzle-Ejector Mixer Thomas Z. Dong; Reda R. Mankbadi Theoretical Analysis and Engineering Modeling of Flowfields in Clustered Module Plug Nozzles Francesco Nasuti; Marcello Onofri Analysis of a Hybrid Dual-Combustion-Chamber Solid-Propellant Gas Generator Jon J. Freesmeier; P. Barry Butler Dynamic Modeling of Hybrid Rocket Combustion M. Arif Karabeyoglu; D. Altman Analyses and Application of Gas Sampling to Scramjet Engine Testing Tohru Mitani; Masahiro Takahashi; Sadatake Tomioka; Tetsuo Hiraiwa; Kouichiro Tani Drags in Scramjet Engine Testing: Experimental and Computational Fluid Dynamics Studies Tohru Mitani; Takeshi Kanda; Tetsuo Hiraiwa; Yasutaka Igarashi; Kazuhiro Nakahashi Closed-Loop Active Control of Combustion Instabilities Using Subharmonic Secondary Fuel Injection C. M. Jones; J. G. Lee; D. A. Santavicca Reduced Kinetics Mechanisms for Ram Accelerator Combustion Eric L. Petersen; Ronald K. Hanson Unified Computer Model for Predicting Thermochemical Erosion in Gun Barrels S. Sopok; P. O'Hara; G. Pflegl; S. Dunn; D. Coats; G. Nickerson Technical Note Determination of Unsteady Heat Release Distribution in Unstable Combustor from Acoustic Pressure Measurements Timothy C. Lieuwen; Yedidia Neumeier; Ben T. Zinn Volume 15 Number 3 May 1999 Full-Length Papers Liquid Jet Atomization in a Compressible Gas Stream Tingbao Chen; Xianguo Li Ion Beamlet Divergence Characteristics of Two-Grid Multiple-Hole IonAccelerator Systems Yukio Hayakawa; Shoji Kitamura Adaptive Control of Combustion Instability with On-Line System Identification Shozo Koshigoe; Toshihiko Komatsuzaki; Vigor Yang Computation of Vortex Shedding in Solid Rocket Motors Using TimeDependent Turbulence Model 390 383 377 369 613 601 591 584 578 572 562 552 544 539 A. Kourta Performance Evaluation of Scramjet Combustors Using Kinetic Energy and Combustion Efficiencies Goro Masuya; Tomokazu Uemoto; Yoshihiro Wakana; Kenji Kudou; Atsuo Murakami; Tomoyuki Komuro Design of Three-Dimensional Hypersonic Inlets with Rectangular-toElliptical Shape Transition M. K. Smart Free-Flight Experiment and Numerical Simulation for Cold Thruster Plume M. S. Ivanov; G. N. Markelov; Yu. I. Gerasimov; A. N. Krylov; L. V. Mishina; E. I. Sokolov Startup Modeling of the Receiver of NASA's 2-Kilowatt Solar Dynamic Power System Guido W. Lopez Experimental Investigation of the Role of Downstream Ramps on a Supersonic Injection Plume Mark P. Wilson; Rodney D. W. Bowersox; Diana D. Glawe Low-Power Helium Pulsed Arcjet Gary F. Willmes; Rodney L. Burton Comparative Study of Coupled-Mode Flutter-Analysis Methods for Fan Configurations R. Srivastava; T. S. R. Reddy Predicted Combined Effects of Purge Flow and Rotor-Casing Eccentricity on Ingress Heating Zhou Guo; David L. Rhode Modified Through-Flow Wave-Rotor Cycle with Combustor-Bypass Ducts Daniel E. Paxson; M. Razi Nalim Launch Vehicle Dynamic and Control Effects from Solid Rocket Motor Slag Ejection K. W. Dotson; J. W. Murdock; D. K. Kamimoto Technical Papers Biharmonic Three-Dimensional Grid Generation for Axial Turbomachinery with Tip Clearance G. A. Gerolymos; G. Tsanga Technical Notes Adaptive Analysis of Oscillating Cascade Flows on a QuadrilateralTriangular Mesh S. Y. Yang Theoretical Prediction of Mean Droplet Size of Y-Jet Atomizers H. S. Couto; J. A. Carvalho Jr.; M. Q. McQuay; P. T. Lacava Optimal Performance of Enthalpy Rocket Lorenzo Casalino; Guido Colasurdo 485 481 479 476 468 462 454 447 440 432 424 417 408 401 Volume 15 Number 2 – Not Available Volume 15 Number 1 – Not Available Volume 14 Number 6 – Not Available Volume 14 Number 5 September 1997 Editorial Another Landmark Collection R. H. Woodward Waesche Space Propulsion Development for the 21st Century Xinmin Ren Preface Vigor Yang; Guoqiu Liu; William E. Anderson; Mohammed Habiballah Full-Length Papers Cycles for Earth-to-Orbit Propulsion Detlef Manski; Christoph Goertz; Hagen-D. Saßnick; James R. Hulka; B. David Goracke; Daniel J. H. Levack Combined Rocket and Airbreathing Propulsion Systems for SpaceLaunch Applications Russell Daines; Corin Segal Preliminary Analysis of an Airbreathing and Rocket Combined-Cycle Engine Feng Qi; Jue Wang; Chien-Pin Chen Advanced Rocket Nozzles Gerald Hagemann; Hans Immich; Thong Van Nguyen; Gennady E. Dumnov Dynamic Amplification of Fluid Pressure in a Propellant Feed Line T. V. Nguyen; W. E. Huffman Propellant Technologies: Far-Reaching Benefits for Aeronautical and Space-Vehicle Propulsion Bryan Palaszewski; Leonid S. Ianovski; Patrick Carrick Propellant Management in Booster and Upper-Stage Propulsion Systems Mark F. Fisher Liquid-Propellant Rocket Engine Health-Monitoring Techniques Yulin Zhang; Jianjun Wu; Minchao Huang; Hengwei Zhu; Qizhi Chen Quality Issues in Propulsion John P. McCarty; Garry M. Lyles Status and Issues Related to In-Space Propulsion Systems R. L. Sackheim; D. C. Byers Nontoxic Orbital Maneuvering and Reaction Control Systems for Reusable Spacecraft Eric Hurlbert; John Applewhite; Tien Nguyen; Brian Reed; Zhang Baojiong; Wang Yue 676 669 664 657 649 641 635 620 613 605 588 587 586 585 Baojiong; Wang Yue Spacecraft Electric Propulsion - An Overview M. Martinez-Sanchez; J. E. Pollard Electric Propulsion for Solar System Exploration John R. Brophy; Muriel Noca Ion Thruster Development Trends and Status in the United States Paul J. Wilbur; Vincent K. Rawlin; J. R. Beattie Pulsed Plasma Thruster R. L. Burton; P. J. Turchi Main Physical Features and Processes Determining the Performance of Stationary Plasma Thrusters Vladimir Kim Scaling of Thrust in Self-Field Magnetoplasmadynamic Thrusters Edgar Choueiri Technology and Application Aspects of Applied Field Magnetoplasmadynamic Propulsion Gerd Krülle; Monika Auweter-Kurtz; Akihiro Sasoh High-Power Hydrogen Arcjet Thrusters Monika Auweter-Kurtz; Thomas Gölz; Harald Habiger; Frank Hammer; Helmut Kurtz; Martin Riehle; Christian Sleziona Experimental Performance of Field Emission Microthrusters Salvo Marcuccio; Angelo Genovese; Mariano Andrenucci Research as a Key in the Design Methodology of Liquid-Propellant Combustion Devices M. Habiballah; L. Vingert; V. Duthoit; P. Vuillermoz Investigation of Heat Transfer and Coking Characteristics of Hydrocarbon Fuels Keming Liang; Baoe Yang; Zhongli Zhang Liquid-Propellant Rocket Engine Injector Dynamics Vladimir G. Bazarov; Vigor Yang Mixing and Spray Formation in Coaxial Jets Emmanuel Villermaux Effects of Periodic Atomization on Combustion Instability in LiquidFueled Propulsion Systems W. E. Anderson; K. L. Miller; H. M. Ryan; S. Pal; R. J. Santoro; J. L. Dressler Experimental Investigation of Shear Coaxial Cryogenic Jet Flames S. Candel; G. Herding; R. Synder; P. Scouflaire; C. Rolon; L. Vingert; M. Habiballah; F. Grisch; M. Péalat; P. Bouchardy; D. Stepowski; A. Cessou; P. Colin Atomization and Breakup of Cryogenic Propellants Under HighPressure Subcritical and Supercritical Conditions Wolfgang O. H. Mayer; Axel H. A. Schik; Bruno Vielle; Christian Chauveau; Iskender Gökalp; Douglas G. Talley; Rodger D. Woodward 835 826 818 807 797 789 782 774 764 754 744 736 716 708 700 688 Chauveau; Iskender Gökalp; Douglas G. Talley; Rodger D. Woodward Modeling High-Pressure Mixing and Combustion Processes in Liquid Rocket Engines Joseph C. Oefelein; Vigor Yang Technical Notes Volume 14 Number 4 July 1998 Full-Length Papers Modified Fracture Mechanics Approach in Structural Analysis of SolidRocket Motors Sook-Ying Ho; Gerard Carè Experimental Study on Boron-Potassium Nitrate Initiated by Shock Liqiong Wang; Changgen Feng; Changsheng Han Measurement System for Determining Solid Propellant Burning Rate Using Transmission Microwave Interferometry Vladica S. Bozic; Djordje D. Blagojevic; Bozidar A. Anicin 429 P. G. Harris; A. De Champlain Modeling and Estimation for Electromechanical Thrust Vector Control of Rocket Engines Dale E. Schinstock; Douglas A. Scott; Tim A. Haskew Investigation of a Solid Fuel Scramjet Combustor Adela Ben-Yakar; Benveniste Natan; Alon Gany Flame-Holding Configurations for Kerosene Combustion in a Mach 1.8 Airflow Michael G. Owens; Sharam Tehranian; Corin Segal; Viatcheslav A. Vinogradov New Model for Intense Self-Similar Vortices Georgios H. Vatistas Shock-Loss Model for Transonic and Supersonic Axial Compressors with Curved Blades M. T. Schobeiri Properties of Laminar Premixed Hydrocarbon/Air Flames at Various Pressures M. I. Hassan; K. T. Aung; O. C. Kwon; G. M. Faeth Strategies for Pulsed Detonation Engine Performance Optimization J.-L. Cambier; J. K. Tegnér Reflections on Free-Piston Stirling Engines, Part 1: Cyclic Steady Operation F. De Monte; G. Benvenuto Reflections on Free-Piston Stirling Engines, Part 2: Stable Operation F. De Monte; G. Benvenuto Generic Magnetic Fusion Rocket Model 519 509 499 489 479 470 462 456 447 440 421 416 409 858 843 John F. Santarius; B. Grant Logan Simplified Approach to Performance Evaluation of Nuclear and Electrical Propulsion Systems Fernando De Souza Costa; João Andrade De Carvalho Jr Vortex Formation and Stability in a Scaled Gas-Core Nuclear Rocket Configuration L. E. Thode; M. C. Cline; S. D. Howe Slingatron Mass Launchers Derek A. Tidman Effect of Propellant Temperature on Efficiency in the Pulsed Plasma Thruster Gregory G. Spanjers; Jamie B. Malak; Robert J. Leiweke; Ronald A. Spores Propellant Losses Because of Particulate Emission in a Pulsed Plasma Thruster Gregory G. Spanjers; Jason S. Lotspeich; Keith A. McFall; Ronald A. Spores Arcjet Anode Plasma Measurements Using Electrostatic Probes Nicholas T. Tiliakos; Rodney L. Burton; Herman Krier Beamlet Profiles from Multiple-Hole Ion-Extraction Systems Yukio Hayakawa; Shoji Kitamura; Katsuhiro Miyazaki Technical Notes Volume 14 Number 3 May 1998 Full-Length Papers Study on Trapped-Vortex Combustor - Effect of Injection on Flow Dynamics Viswanath R. Katta; W. M. Roquemore Transition Characteristics of Flowfield in a Simulated Solid-Rocket Motor Tong-Miin Liou; Wan-Yih Lien; Po-Wen Hwang Determination of Pressure Dependence of Burning Rate in Solid Motors Using Ultrasonic Technique Desh Deepak; R. Jeenu; P. Sridharan; M. S. Padmanabhan Effect of Catalyst Addition on Subatmospheric Burning Surface Temperature of Composite Propellants S. Krishnan; R. D. Swami Temperature and Species Measurements in a Low-Thrust Hydrogen/Oxygen Rocket Engine Wilhelmus A. de Groot Model of Turbulent Mixing and Reaction for H2-Air Combustion Marc A. Cremer; Patrick A. McMurtry Methodology to Solve Flowfields of Plug Nozzles for Future Launchers 318 309 301 295 290 282 273 575 568 560 554 545 537 530 525 Francesco Nasuti; Marcello Onofri Transport-Property Measurements in the Plume of an SPT-100 Hall Thruster Lyon B. King; Alec D. Gallimore; Colleen M. Marrese Surface Modification Measurements in the T5 Ion Thruster Plume L. Najeeb Ahmed; Mark W. Crofton Load Oscillations Caused by Unstart of Hypersonic Wind Tunnels and Engines Takashi Shimura; Tohru Mitani; Noboru Sakuranaka; Muneo Izumikawa Symmetry Approach to Extension of Flutter Boundaries via Mistuning B. Shapiro Numerical Simulation of Incompressible Two-Blade Rotor Flowfields John A. Ekaterinaris Stability Behavior of a Shaft-Disk System Subjected to Longitudinal Force Lien-Wen Chen; Hong-Cheng Sheu Heat Transfer in Counterswirled Coaxial Jet Mixing J. L. Sanger; P. A. Dellenback Sound-Pressure-Level Variations in a Supersonic Rectangular Cavity at Yaw Peter J. Disimile; Paul D. Orkwis Application of Two-Variable Fuzzy-PI Control in an Aeroengine Fang Zhongxiang; Wu Chihua Analysis of Ar-Cs Magnetohydrodynamics Disk Generator with Strong Interaction Motoo Ishikawa; Takuro Shiomi; Yoshitaka Inui; Hiroyuki Yamasaki Volume 14 Number 2 March 1998 Full-Length Papers Jet-Engine Test Cell Augmenter Performance C. A. Kodres; G. L. Murphy Comparison of Physical and Aerodynamic Ramps as Fuel Injectors in Supersonic Flow Raymond P. Fuller; Pei-Kuan Wu; Abdollah S. Nejad; Joseph A. Schetz Investigation of Cryogenic Propellant Flames Using Computerized Tomography of Emission Images Gerald Herding; Ray Snyder; Carlos Rolon; Sebastien Candel Competitive Reactivity of Stabilizers and Ballistic Modifiers During Simulated Aging of Propellants M. H. Sammour Leading-Edge Flame Detachment: Effect on Pressure-Coupled Combustion Response 160 152 146 135 129 403 399 392 384 375 367 354 348 336 327 C. A. Beiter; E. W. Price Ignition Dynamics of Boron Particles in a Shock Tube Herman Krier; R. L. Burton; M. J. Spalding; T. J. Rood Spray Structures of Liquid Jets Atomized in Subsonic Crossflows Pei-Kuan Wu; Kevin A. Kirkendall; Raymond P. Fuller; Abdollah S. Nejad Three-Dimensional Turbine Rotor Forcing Functions and Linear Theory Analysis David A. Johnston; Sanford Fleeter Measured Rotor Wake and Potential Forcing Functions, Including Blade Row Interactions Robert T. Johnston; John M. Feiereisen; Sanford Fleeter Blading Response to Potential Field Interactions in Axial- and RadialFlow Turbomachinery Albert J. Sanders; Sanford Fleeter Preliminary Estimation of Engine Gas-Flow-Path Size and Weight Vivek Sanghi; S. Kishore Kumar; V. Sundararajan; S. K. Sane Wake Decay: Effect of Freestream Swirl J. M. Brookfield; I. A. Waitz; J. Sell Aerodynamic Shape Optimization of a Subsonic Inlet Using ThreeDimensional Euler Computation D. R. Reddy; E. S. Reddy; R. E. Moody Overexpanded Two-Dimensional Convergent-Divergent Nozzle Performance, Effects of Three-Dimensional Flow Interactions A. Hamed; C. Vogiatzis Aerodynamics Performance Prediction of Thrust-Vectoring Nozzles A. Matesanz; A. Velazquez; M. Rodriguez Propellant Utilization in Hall Thrusters Y. Raitses; J. Ashkenazy; M. Guelman Quasisteady Ablative Magnetoplasmadynamic Thruster Performance with Different Propellants Giorgio Paccani; Ugo Chiarotti; William D. Deininger Laser Propulsion System for Space Vehicles Aviad Brandstein; Yeshayahou Levy Technical Notes Rocket Propulsion Strategy Based on Kinetic Energy Management Merrill K. King Volume 14 Number 1 January 1998 Editorial Full-Length Papers 1 270 261 254 247 241 234 225 215 208 199 191 183 173 166 Reacting Flow Establishment in Ram Accelerators: A Numerical Study S. Yungster; K. Radhakrishnan; M. J. Rabinowitz Control of Flame-Holding in Supersonic Airflow by Secondary Air Injection Shuhei Takahashi; Naohiro Sato; Mitsuhiro Tsue; Michikata Kono; Masahiko Nakamura; Hiroshi Kondo; Yasushige Ujiie Improved Physics Model for the Gasdynamic Mirror Fusion Propulsion System Terry Kammash; David L. Galbraith Modeling Plasma Processes in 1-Kilowatt Hydrazine Arcjet Thrusters Thomas W. Megli; Junqing Lu; Herman Krier; Rodney L. Burton Thermal Decomposition of 3,3_-Bis-Azidomethyl-Oxetane Young Joo Lee; Ching-Jen Tang; Gautam Kudva; Thomas A. Litzinger Droplet Combustion, Microexplosion, and Sooting Characteristics of Several Energetic Liquid Propellants T. X. Li; D. L. Zhu; C. K. Law Characterization of Fuel Regression in a Radial Flow Hybrid Rocket J. R. Caravella Jr; S. D. Heister; E. J. Wernimont Characteristics of a Trapped-Vortex Combustor K.-Y. Hsu; L. P. Goss; W. M. Roquemore Assessment of a Radiative Heat Transfer Model for Gas Turbine Combustor Preliminary Design Peter J. Stuttaford; Philip A. Rubini Digital Simulator for Steady-State Performance Prediction of Military Turbofan Engine Vivek Sanghi; B. K. Lakshmanan; V. Sundararajan Influence of Inlet Pressure Distortion on a Convertible Engine Fan Tarik Kaya Numerical Investigation of Inlet Buzz Flow Pong-Jeu Lu; Ling-Tzong Jain Method for Noise Suppressing Nozzle Calculation and First Results of Its Implementation S. Bosniakov; S. Fonov; V. Jitenev; A. Shenkin; V. Vlasenko; N. Yatskevich Experimental Analysis of the Turbulent Shear Stresses for Distorted Supersonic Boundary Layers Joel J. Luker; Chad S. Hale; Rodney D. W. Bowersox Solar Cell Temperature on Mars E. Matz; J. Appelbaum; Y. Taitel; D. J. Flood Mars Dust-Removal Technology Geoffrey A. Landis 10 18 24 29 37 45 51 57 66 74 82 90 101 110 119 126 Volume 13 Number 6 November 2001 FULL-LENGTH PAPERS Study of a Supersonic Combustor Employing Swept Ramp Fuel Injectors Dean R. Eklund; Scott D. Stouffer; G. Burton Northam Open-Loop Performance of a Fast-Response, Actively Controlled Fuel Injector Actuator Yedidia Neumeier; Aharon Nabi; Amos Arbel; Moti Vertzberger; Ben T. Zinn Effects of Inlet Configuration on Ignition and Fuel Regression Behind a Backstep Cliff Yuh-Yih Wu; Jing-Tang Yang Laser-Induced Spark Flameholding in Supercritical, Subsonic Flow Lara D. Medoff; Andrew McIlroy Uncertainty Assessment of Ramjet Performance Determination in Connected-Pipe Testing John A. Blevins; Hugh W. Coleman Assessment of Jet Noise Analysis Codes for Multistream Axisymmetric and Forced Mixer Nozzles T. J. Barber; L. M. Chiappetta; S. H. Zysman Zonal Approach for Prediction of Jet Noise S. H. Shih; D. R. Hixon; R. R. Mankbadi Effect of Wall Roughness on the Flow Through Converging - Diverging Nozzles Venkata S. Krishnamurty; Wei Shyy Absolute Instability in a Supersonic Shear Layer and Mixing Control Long-Shin Lee; Philip J. Morris Velocity and Temperature Measurements in a Low-Power Hydrazine Arcjet S. A. Bufton; R. L. Burton Extensive Validation of a Monte Carlo Model for Hydrogen Arcjet Flowfields Iain D. Boyd Measurements of Electron Density in the Charge Exchange Plasma of an Ion Thruster P. C. T. De Boer Numerical Analysis of a Two-Dimensional Magnetoplasmadynamic Arcjet I. Funaki; K. Toki; K. Kuriki Prediction of Pressurant Mass Requirements for Axisymmetric Liquid Hydrogen Tanks Neil T. Van Dresar TECHNICAL NOTES Cored Brick Storage Heater Analysis 800 796 789 783 775 768 763 753 745 737 730 721 714 705 697 Robert H. Korkegi Operation of Quasi-Two-Dimensional Projectiles in a Ram Accelerator Xinyu Chang; Andrew Higgins; Eric Schultz; Adam Bruckner Further Examination of Enthalpy Rocket Performance Merrill K. King Effects of Kinetic Rate Uncertainty on the Predicted Performance of Solar Thermal Rockets D. Brian Landrum; Robert M. Beard Off-Design Performance Prediction of Single-Spool Turbojets Using Gasdynamics Mirza F. Baig; H. I. H. Saravanamuttoo ERRATA Compatibility of Gelled Inhibited Red Fuming Nitric Acid with Aluminum Alloys Barry D. Allan; and Volume 13 Number 5 September 2001 FULL-LENGTH PAPERS Challenge to Create the Space Drive Marc G. Millis Performance Limits for Projectile Flight in the Ram and External Propulsion Accelerators J. Rom Performance Optimization of a Supersonic Combustion Ram Accelerator Projectile John W. Sabean; Mark J. Lewis Analytical Solution of the Type IV Shock Interaction Michael J. Frame; Mark J. Lewis Applications of Algebraic Reynolds Stress Turbulence Models Part 1: Incompressible Flat Plate John R. Carlson Applications of Algebraic Reynolds Stress Turbulence Models Part 2: Transonic Shock-Separated Afterbody John R. Carlson Plug Nozzle Flowfield Analysis T. Rommel; G. Hagemann; C.-A. Schley; G. Krülle; D. Manski Comparison of Scramjet Engine Performance in Mach 6 Vitiated and Storage-Heated Air Tohru Mitani; Tetsuo Hiraiwa; Shigeru Sato; Sadatake Tomioka; Takeshi Kanda; Kouichiro Tani Flammability Limits and Probability Density Functions in Simulated Solid-Fuel Ramjet Combustors Tong-Miin Liou; Wan-Yih Lien; Po-Wen Hwang 643 635 629 620 610 601 592 583 577 811 808 806 804 802 Performance and Acceleration Process of Quasisteady Magnetoplasmadynamic Arcjets with Applied Magnetic Fields Hirokazu Tahara; Yoichi Kagaya; Takao Yoshikawa Experimental Study of Hydrogen Heating in Powerful Electric Discharge Launcher Ph. G. Rutberg; A. A. Bogomaz; A. V. Budin; V. A. Kolikov; A. G. Kuprin; A. A. Pozubenkov Jet Engine Component Maps for Performance Modeling and Diagnosis G. Sieros; A. Stamatis; K. Mathioudakis High-Temperature Braided Rope Seals for Static Sealing Applications Bruce M. Steinetz; Michael L. Adams; Paul A. Bartolotta; Ram Darolia; Andrew Olsen Identification of Continuous-Time, Linear, and Nonlinear Models of an Electromechanical Actuator Dale E. Schinstock; Tim A. Haskew Theoretical Formulation for Sauter Mean Diameter of Pressure-Swirl Atomizers H. S. Couto; J. A. Carvalho Jr; D. Bastos-Netto Volume 13 Number 4 July 1997 FULL-LENGTH PAPERS Measurement System for Determining Solid Rocket Propellant Burning Rate Using Reflection Microwave Interferometry Vladica S. Bozic; Djordje Dj. Blagojevi; Bozidar A. Anicin High-Speed Photographic Study of the Impact Response of Ammonium Dinitramide and Glycidyl Azide Polymer J. P. Agrawal; S. M. Walley; J. E. Field Mechanism of Burning Rate Enhancement of Composite Solid Propellants by Ferric Oxide Satyanarayanan R. Chakravarthy; Edward W. Price; Robert K. Sigman Compatibility of Gelled Inhibited Red Fuming Nitric Acid with Aluminum Alloys Ramona E. Arndt Hallit; Clark W. Hawk Experimental Study on Rotating Cavitation of Rocket Propellant Pump Inducers T. Hashimoto; M. Yoshida; M. Watanabe Hybrid Friction - Impact Vibration Damper for Cryogenic Rotating Machinery J. Jeffrey Moore; Alan B.; Ravindera K. Gadangi Mean Stator Loading Effect on the Acoustic Response of a Rotating Cascade Scott Sawyer; Sanford Fleeter Macroscopic Balance Model for Wave Rotors Gerard E. Welch 651 659 665 675 683 691 457 463 471 481 488 495 502 508 Turbulent Mixing of Coaxial Nozzle Flows with a Central-Lobed Mixer S. C. M. Yu; X. G. Xu Effects of Mixing Schemes on Kerosene Combustion in a Supersonic Airstream M. Owens; C. Segal; A. H. Auslender Hydrogen Autoignition and Combustion in Supersonic Flow at Low Equivalence Ratio Giulio Riva; Giambattista Daminelli; Adolfo Reggiori Experimental Studies on Self-Ignition of Hydrogen/Air Supersonic Combustion Li Jian-Guo; Yu Gong; Zhang Yue; Li Ying; Qian Da-Xing Mach 6 Testing of a Scramjet Engine Model Takeshi Kanda; Tetsuo Hiraiwa; Tohru Mitani; Sadatake Tomioka; Nobuo Chinzei Uncertainty Assessment of Performance Evaluation Methods for Solar Thermal Absorber/Thruster Testing Pete Markopoulos; Hugh W. Coleman; Clark W. Hawk Solar Space Power System Optimization with Ultralight Radiator A. F. Massardo; L. A. Tagliafico; M. Fossa; A. Agazzani Biphase Inverter Based on Cesium Plasma Switches N. I. Alekseyev; V. B. Kaplan; A. M. Martsinovskij; S. V. Electrov United States Laboratory Element Electrical Power System Verification Approach Herb W. Wallen; S. Johnny Fu TECHNICAL NOTES Thrust Enhancement in Hypervelocity Nozzles by Chemical Catalysis D. J. Singh; Mark H. Carpenter; J. P. Drummond Volume 13 Number 3 May 1997 Full-Length Papers Unsteady Aerodynamic Flow Phenomena in a Transonic Compressor Stage Chunnil Hah; Steven L. Puterbaugh; William W. Copenhaver Modular Prediction Scheme for Blade Row Interaction Noise A. B. Parry Skin-Friction Predictions in a Crossing-Shock Turbulent Interaction Datta Gaitonde; J. S. Shang Stability Testing of Full-Scale Tactical Motors F. S. Blomshield; J. E. Crump; H. B. Mathes; Richard A. Stalnaker; M. W. Beckstead Nonlinear Stability Testing of Full-Scale Tactical Motors F. S. Blomshield; H. B. Mathes; J. E. Crump; C. A. Beiter; M. W. Beckstead 517 525 532 538 543 552 560 565 570 574 329 334 342 349 356 Beckstead Modeling and Experiments of Laser-Induced Ignition of Nitramine Propellants S. J. Ritchie; S. T. Thynell; K. K. Kuo Improvements to Steady-State Combustion Modeling of Cyclotrimethylenetrinitramine Jeffrey E. Davidson; M. W. Beckstead Fiber-Optic Probe for Laser-Induced Fluorescence Measurements of the Fuel-Air Distribution in Gas-Turbine Combustors Jong Guen Lee; Domenic A. Santavicca Optical and Pressure Measurements in Shock Tunnel Testing of a Model Scramjet Combustor T. J. McIntyre; A. F. P. Houwing; P. C. Palma; P. A. B. Rabbath; J. S. Fox Comparison of Potential Fuels for Martian Rockets Using CO2 Evgeny Ya. Shafirovich; Udo I. Goldshleger Partial Differential Equation Surface Generation and Functional Shape Optimization of a Swirl Port C. W. Dekanski; M. I. G. Bloor; M. J. Wilson Thermal Analysis of the Heat Exchangers and Regenerator in Stirling Cycle Machines Filippo de Monte Counterflow Thrust Vector Control of Subsonic Jets: Continuous and Bistable Regimes M. R. Van der Veer; P. J. Strykowski High-Thrust-High-Specific Impulse Gasdynamic Fusion Propulsion System Terry Kammash; Myoung-Jae Lee; David I. Poston Antiproton Catalyzed Fusion Propulsion for Interplanetary Missions B. N. Cassenti; T. Kammash; D. L. Galbraith Fundamental Constraints on Large-Scale Antimatter Rocket Propulsion Todd H. Rider Technical Notes Overexpanded Two-Dimensional-Convergent-Divergent Nozzle Flow Simulations, Assessment of Turbulence Models A. Hamed; C. Vogiatzis Lobed Mixers Using Simultaneous Laser-Induced Fluorescence and Mie Scattering David M. Milam; Mo Samimy; Steven Martens Combustion and Microexplosion of Han-Based Liquid Gun Propellants at Elevated Pressures C. Call; D. L. Zhu; C. K. Law; S. C. Deevi Interpretation of Finite Element Analysis Results of Scramaccelerator Thrust 451 448 445 444 435 428 421 412 404 398 395 388 384 375 367 Josef Rom; Mark J. Lewis Technical Comments Comment on "Intrinsic Combustion Instability of Solid Energetic Materials" M. Q. Brewster; S. F. Son Reply by the Author to M. Q. Brewster and S. F. Son L. DeLuca Volume 13 Number 2 March 1997 Full-Length Papers Exit Flowfield of an Embedded Stator in a Multistage Axial Flow Compressor J. Prato; B. Lakshminarayana; N. Suryavamshi Gust Response Decomposition in a Stator/Rotor Axial Compressor with Varying Axial Gap Andrew M. Wo; Meng-Hsuan Chung; Shu-Tzung Hsu Multiple-Scales Solution to the Acoustic Boundary Layer in Solid Rocket Motors J. Majdalani; W. K. van Moorhem Flow Analysis of a Solid Propellant Rocket Motor with Aft Fins Bruno Chaouat Vortex Shedding in a Large Solid Rocket Motor Without Inhibitors at the Segment Interfaces K. W. Dotson; S. Koshigoe; K. K. Pace Effect of Catalyst Mixing Procedure on Subatmospheric Combustion Characteristics of Composite Propellants S. Krishnan; R. D. Swami Combustion Initiated by a Porous Ceramic Regenerator in a Reciprocating Engine Environment Steven Sepka; Francisco Ruiz Monte Carlo Probability Density Function Method for Gas Turbine Combustor Flowfield Predictions Anil K. Tolpadi; Sanjay M. Correa; David L. Burrus; Hukam C. Mongia Partially Premixed Laminar Gas Flames from Triangular Burners S. R. Gollahalli; Samir Subba Counterflow Diffusion Flame of Methane and Methane/Hydrogen Mixed Fuel in Supersonic Flow Kenichi Takita; Takashi Niioka Properties of Laminar Premixed CO/H2/Air Flames at Various Pressures M. I. Hassan; K. T. Aung; G. M. Faeth Ignition Characteristics of a New High-Energy Density Fuel in HighSpeed Flows 246 239 233 226 218 213 207 197 194 186 178 169 456 454 C. Segal; M. J. Friedauer; H. S. Udaykumar; W. Shyy; A. P. Marchand Spray Characteristics of Liquid Jet Traversing Subsonic Airstreams Takao Inamura; Nobuki Nagai Normal, Sonic Helium Injection Through a Wedge-Shaped Orifice into Supersonic Flow Matthew J. Barber; Joseph A. Schetz; Larry A. Roe Velocity Measurements of a Jet Injected into a Supersonic Crossflow Juan Gabriel Santiago; J. Craig Dutton Fuel Stagnation Temperature Effects on Mixing with Supersonic Combustion Flows M. N. Wendt; R. J. Stalker; P. A. Jacobs Thrust Losses in Hypersonic Engines Part 1: Methodology D. W. Riggins; C. R. McClinton; P. H. Vitt Thrust Losses in Hypersonic Engines Part 2: Applications D. W. Riggins Evaluation of Performance Loss Methods for High-Speed Engines and Engine Components D. W. Riggins Mixing Characteristics of Forced Mixers with Scalloped Lobes Simon C. M. Yu; T. H. Yip; C. Y. Liu Flow Through a Rectangular-to-Semiannular Diffusing Transition Duct Jeff Foster; Bruce J. Wendt; Bruce A. Reichert; Theodore H. Okiishi Power System Analysis of Multikilowatt Space/Planet Stations George L. Kusic; Ronald C. Cull Technical Notes Volume 13 Number 1 January 1997 Editorial Full-Length Papers Analytical Model of Unsteady Shock Motion on Hypersonic Forebodies Sowmyalatha Jayaraman; Mark J. Lewis Unsteady Flow and Shock Motion in a Transonic Compressor Rotor W. W. Copenhaver; S. L. Puterbaugh; C. Hah Tip Clearance Flow-Shock Interaction in a Transonic Compressor Rotor S. L. Puterbaugh; M. Brendel Computational Study of Rotating-Stall Inception in Axial Compressors L. He Chordwise Bending Cascade Unsteady Aerodynamics by an Experimental Influence Coefficient Technique Daniel A. Ehrlich; Sanford Fleeter 39 31 24 17 10 1 324 318 312 305 296 288 281 274 264 257 250 Secondary Flow Computation Using an Inviscid Multigrid Finite Volume Lambda Formulation Francesco Casalini; Andrea Dadone Tangential Injection from Overlaid Slots into a Supersonic Stream David P. Lewis; Joseph A. Schetz Breakup Processes of Liquid Jets in Subsonic Crossflows Pei-Kuan Wu; Kevin A. Kirkendall; Raymond P. Fuller; Abdollah S. Nejad Stability of Thin Liquid Sheet Flows Marc W. McConley; Donald L. Chubb; Matthew S. McMaster; Abdollah A. Afjeh Effect of Acoustic Perturbations on Liquid Jet Atomization S. D. Heister; M. W. Rutz; J. H. Hilbing Droplet Autoignition in a Reactive Oxidant/Fuel-Vapor/Inert Environment Xianguo Li Mass-Flux-Based Implicit Multigrid Method for Modeling Multidimensional Combustion Xiaoqing Zheng; Changming Liao; Zhining Liu; Chaoqun Liu Comparison Between Presumed and Monte Carlo Probability Density Function Combustion Models Fernando Biagioli Prediction of Soot Emissions in Gas-Turbine Combustors A. de Champlain; D. Kretschmer; J. Tsogo; G. F. Pearce Multidimensional Modeling of Fuel Effects and Split Injections on Diesel Engine Cold-Starting Nabil S. Ayoub; Rolf D. Reitz Numerical Study of Hypervelocity Flows Through a Scramjet Combustor R. Krishnamurthy; R. C. Rogers; S. N. Tiwari Experimental Studies on Piloted Supersonic Combustion Using the Petal Nozzle Anil K. Narayanan; K. A. Damodaran Mixed Integer Programming-Based Power Scheduler for the Space Station James Momoh; D. Chattopadhyay; James L. Dolce Optimal Control of Quasi-One-Dimensional Self-Field Magnetoplasmadynamic Arcjet Flowfields Kyoichiro Toki Technical Notes Technical Comments 49 59 64 74 82 89 97 109 117 123 131 142 150 157 162 167