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AHS 66th Annual Forum
& Technology Display –
Rising to New Heights in Vertical Flight Technology
May 11-13, 2010
Phoenix, Arizona
TECHNICAL SESSIONS
Technical Sessions FORUM 66
A: TUESDAY, MAY 11 – MORNING
Aerodynamics I Advanced Vertical Crash Safety I History
8:00 a.m. – 12:00 noon Flight I 8:00 a.m. – 11:30 a.m. 8:00 a.m. – 12 noon
Room 164 8:00 a.m. – 12 noon Room 160 Room 161
Session Chair: Glen Whitehouse, Room 166 Session Chair: David Laananen, Session Chair: J. Gordon Leishman,
Continuum Dynamics, Inc. Session Chair: Naipei (Peter) Bi, Arizona State University (Ret.) University of Maryland
U. S. Navy
Paper #1 – 8:00 a.m. – 8:30 a.m. Paper #1 -- 8:00 a.m. – 8:30 a.m. Paper #1 – 8:00 a.m. – 8:30 a.m. Paper #1 – 8:00 a.m. – 8:30 a.m. *
CH-53K Scale Model Aerodynamic Fancraft: Extending the Reach of System-Integrated Finite Element The Rotorcraft Career of Prof.
Evaluation Aviation Analysis of a Full-Scale Helicopter Norman D. Ham (or what
P. F. Lorber, J. O'Neil, F. Kohlhepp, J. R. Yoeli, Urban Aeronautics Ltd. Crash Test with Deployable Energy Individual Blade Control Really
Cantono, A. Bagai, R. C. Moffitt, Absorbers Means)
Sikorsky Aircraft Corporation and S. M. Annett, NASA Langley Research W. Johnson and R. M. McKillip, Jr.,
Woods, NAVAIR Center and M. Polanco, ATK Space NASA Ames Research Center
Systems
Paper #2 – 8:30 a.m. – 9:00 a.m. Paper #2 -- 8:30 a.m. – 9:00 a.m. Paper #2 – 8:30 a.m. – 9:00 a.m. Paper #2 – 8:30 a.m. – 9:00 a.m.
Aerodynamic Investigations on a Experiments of Ducted Lift Fans Full Scale Crash Test of an MD- Weir Autogiros and Helicopters
Helicopter Main Rotor Hub in Hover and Edgewise Flight 500 Helicopter with Deployable J.-P. Harrison, Consultant
F. Vogel, C. Breitsamter, N.A. L. Myers, R. Hook, D. McLaughlin, Energy Absorbers
Adams, Technische Universität The Pennsylvania State University S. Kellas, K. Jackson, NASA Langley
München Research Center and J. Littell, ATK
Space Systems
Paper #3 – 9:00 a.m. -9:30 a.m. Paper #3 – 9:00 a.m. – 9:30 a.m. Paper #3 – 9:00 a.m. – 9:30 a.m. Paper #3 – 9:00 a.m. – 9:30 a.m. (+)
Physics-Based Analysis Influence of Tip Clearance and Evaluation of Smooth Particle Czechoslovakian, Polish and
Methodology for Hub Drag Inlet Flow Distortion on Ducted Hydrodynamic Methods for the Yugoslavian V/STOL Concepts of
Prediction Fan Rotor Performance in VTOL Simulation of Helicopter Ditching the 20th Century
J. O. Bridgeman and G. T. UAVs N. Toso-Pentecôte and C. M. Hirshberg, CENTRA Technology,
Lancaster, Bell Helicopter Textron, A. Akturk and C. Camci, The Kindervater, DLR, D. Delsart, Inc., T. Müller, Aviation Historian,
Inc. Pennsylvania State University ONERA, and A. Vagnot, Eurocopter and M. Furda, Aviation Historian
Refreshments Refreshments Refreshments Refreshments
9:30 a.m. – 10:00 a.m. 9:30 a.m. – 10:00 a.m. 9:30 a.m. – 10:00 a.m. 9:30 a.m. – 10:00 a.m.
Paper #4 – 10:00 a.m. – 10:30 a.m. Paper #4 – 10:00 a.m. – 10:30 a.m. Paper #4 – 10:00 a.m. – 10:30 a.m. Paper #4 – 10:00 a.m. – 10:30 a.m. (+)
Analysis of a Hovering Rotor in Conceptual Design of a Hover- Energy Absorption of Sandwiched Wrecked Rotors: Understanding
Icing Conditions Capable High-Speed Multi-Role Honeycombs with Facesheets Rotorcraft Accidents, 1935-1945
R. Narducci, The Boeing Company MAV under In-plane Crushing R. Connor, Smithsonian Institution
and R. E. Kreeger, NASA Glenn J. Albright and J. Sirohi, University B. Atli-Veltin and F. Gandhi, The
Research Center of Texas at Austin Pennsylvania State University
Paper #5 – 10:30 a.m. – 11:00 a.m. Paper #5 – 10:30 a.m. – 11:00 a.m. Paper #5 – 10:30 a.m. – 11:00 a.m. Paper #5 – 10:30 a.m. – 11:00 a.m.
Validation of a New Rotor Flow Titltrotor / Titltwing Performance Towards a Methodology to Design Engineering Analysis of Nicolas
Code Using JMRTS Experimental Enhancement via Active On-blade Water Impact Crashworthy Florine's Helicopters, 1926–1938
Data Flaps Structures J. G. Leishman, University of
Y. Tanabe and S. Saito, JAXA T. Quackenbush, D. Wachspress, R. E. Francesconi and M. Anghileri, Maryland
McKillip, Jr. and C. Solomon, Politecnico di Milano
Continuum Dynamics, Inc.
Paper #6 – 11:00 a.m. – 11:30 a.m. Paper #6 – 11:00 a.m. – 11:30 a.m. Paper #6 – 11:00 a.m. – 11:30 a.m. Paper #6 – 11:00 a.m. – 11:30 a.m. (+)
Analysis of CFD Modeling Opimally Actuated Spanwise- Development of Applied Dynamic The 1972 Easter Offensive and the
Techniques over the MV-22 Segmented Aerodynamic Effectors Overshoot Factors for Structural Evolution of Army Close Air
Tiltrotor for Rotorcraft Power Reduction Analysis of Rotary Wing Aircraft Support Doctrine
J. Abras, NAVAIR and R. Narducci, E. S. Bae and F. Gandhi, The Crashworthy Seating J. Bernstein, National Guard
The Boeing Company Pennsylvania State University J. Fait, M. Richards and C. Educational Foundation
Whitaker, BAE Systems
Paper #7 – 11:30 a.m. – 12 noon Paper #7 – 11:30 a.m. – 12 noon (+) Paper #7 – 11:30 a.m. – 12 noon
An Evaluation of the Influence of A Cargo Unmanned Aircraft Rotor without Reaction Torque
the Test Facility on Rotor System (Cargo UAS) Design and Historical Review of H.G.Küssner's
Performance Characteristics CONOPS Research
J. R. Cook and M. J. Smith, Georgia D. Baldwin, Baldwin Technology W. Geissler and B. G. van der Wall,
Institute of Technology Company DLR
Legend
(+) Paper on Supplemental CD * Presentation Only • Status Unknown
2
Technical Sessions FORUM 66
A: TUESDAY, MAY 11 – MORNING
IMPACT Operations I Propulsion I Structures and Materials I
8:00 a.m. – 12 noon
8:00 a.m. – 11:00 a.m. 8:00 a.m. – 11:00 a.m. 8:00 a.m. – 12 noon
Room 167
Room 162 Room 165 Room 163
Session Chair: Suresh Moon, L-3
Session Chair: Dan Ursenbach, Session Chair: Suzan DeGarmo, Session Chair: Ryan Ehinger, Bell
Communications
Sikorsky Aircraft Corporation and Sikorsky Aircraft Corp. Helicopter Textron Inc.
Deputy Session Chair Ed Lee, Bell
Helicopter Textron, Inc.
Paper #1 – 8:00 a.m. – 8:30 a.m. Paper #1 – 8:00 a.m. – 8:30 a.m. Paper #1 – 8:00 a.m. – 8:30 a.m. Paper #1 – 8:00 a.m. – 8:30 a.m.
Downselection and Metallurgical Development of the AH-64D Vibration Measurements of an Durability and Damage Tolerance
Evaluation of TI 6AL-4V Direct- Apache Longbow Integration with OH-58D Helicopter Planetary Enhancement Feature and Life
To-Metal Fabrication for Unmanned Aircraft Systems Gear under Operating Conditions Prediction Methodology for the
Aerospace Grade Applications S. Swinsick, The Boeing Company T. M. Ericson, R. G. Parker, Ohio Apache Composite Main Rotor
J. Franklin, Bell Helicopter Textron State University Blade (CMRB) Root-end Fitting
Inc. J. Li, P. Jouin, A. Llanos, The Boeing
Company
Paper #2 – 8:30 a.m. – 9:00 a.m. * Paper #2 – 8:30 a.m. – 9:00 a.m. Paper #2 – 8:30 a.m. – 9:00 a.m.
Use of XworX Innovative Application for the Operations On the Vibration Damping Paper #2 – 8:30 a.m. – 9:00 a.m.
Manufacturing Process Facility in Analysis of Rotorcraft in Control of the Input Section of a An Integrated Rotorcraft Damage
Development of Advanced Rotor Homeland Security, Disaster, and Helicopter Main Drive-train Tolerance Methodology for Design,
Blades Emergency Response Missions System Incorporating Squeeze Film Analysis, and Qualification of
J. D. Hethcock, M. E. Tohlen, and P. T. Gibson, J. R. Barber, Bell Damper Fatigue Critical Metal Airframe
K. Oldroyd, Bell Helicopter Textron Helicopter Textron Inc. S. He and T. Okolo, Sikorsky Structure
Inc. Aircraft Corp. P. Bates, M. Urban, and J. Cycon,
Sikorsky Aircraft Corp.
Paper #3 – 9:00 a.m. – 9:30 a.m. (+) Paper #3 – 9:00 a.m. – 9:30 a.m. Paper #3 – 9:00 a.m. – 9:30 a.m.
Manufacturing Issues and Their Another Burr Under the Saddle. Two-Speed Gearbox Dynamic Paper #3 – 9:00 a.m. – 9:30 a.m.
Effects on Structural Performance Threat, Asymmetric Application Simulation Predictions and Test The Bell Model 429 Composite
of Composite Parts and UAVs Validation Main Rotor Blade Flaw Tolerance
A. Makeev, Y. Nikishkov, and P. COL D. L. Cobs, USMC and COL D. G. Lewicki, NASA Glenn Certification
Carpentier, Georgia Institute of C. Merkt, (R), U.S. Army Research Center, H. DeSmidt, S. R. Johnston, R. C. Watkins, Bell
Technology University of Tennessee, E. C. Helicopter Textron Inc.
Smith, The Pennsylvania State
University, and S. W. Bauman,
NASA Glenn Research Center
Refreshments Refreshments Refreshments Refreshments
9:30 a.m. – 10:00 a.m. 9:30 a.m. – 10:00 a.m. 9:30 a.m. – 10:00 a.m. 9:30 a.m. – 10:00 a.m.
Paper #4 – 10:00 a.m. – 10:30 a.m. Paper#4 – 10:00 a.m. – 10:30 a.m. (+) Paper #4 – 10:00 a.m. – 10:30 a.m. Paper #4 – 10:00 a.m. – 10:30 a.m.
Development of an Improved Deice Developing a 3-D Landing Variable Speed Transmission using Design and Performance
System for UH-60 Rotor Blades Symbology Solution for Brownout a Planetary Gear System for High Optimizations of Advanced
D. Nguyen, Sikorsky Aircraft C. Goff, A. Ball, and J. Yapp, dstl Speed Rotorcraft Application Erosion-Resistant Low
Corporation, R. Bozek, Cox and and S. Pearce and F. Crawford, S. V. Ashok, B. Wade, D. P. Schrage, Conductivity Thermal Barrier
Company, Inc. and L. R. AgustaWestland Georgia Institute of Technology Coatings for Rotorcraft Engines
Centolanza, US Army AATD D. Zhu, R. A. Miller, M. A.
Kuczmarski, NASA Glenn Research
Paper #5 – 10:30 a.m. – 11:00 a.m. Paper #5 – 10:30 a.m. – 11:00 a.m. Paper #5 – 10:30 a.m. – 11:00 a.m. Center
Product Lifecycle Engineering An Automated Approach for the Elastohydrodynamic Lubrication
(PLE): A Manufacturing Objective Evaluation of Practice Analysis of Meshing Conjugate Paper #5 – 10:30 a.m. – 11:00 a.m.
Influenced Design Trade Study Autorotations using Available Face-Gear-Pairs for Pericyclic Static Design Flight Loads with
Application Aircraft Data Transmissions Fly-By-Wire Technology
D. Schrage, Georgia Institute of P. Nguyen, Naval Surface Warfare Z. B. Saribay, R. C. Bill, E. C. Smith, A. A. Leone, Sikorsky Aircraft Corp.
Technology Center, J. Walker, Quadelta, Inc. S. Rao, The Pennsylvania State
and Capt. B. Pierce, USMC, MCAS University
New River, NC
Paper #6 – 11:00 a.m. – 11:30 a.m. * Paper #6 – 11:00 a.m. – 11:30 a.m. •
Paper #6 – 10:30 a.m. – 11:00 a.m. Design and Development of a Materials Characterization of
WAAS Rotorcraft Infrastructure Dual Ratio Transmission for the Cast EV31A-T6 Magnesium for
Development & Public Use Next A160T UAV Rotorcraft Rotorcraft Applications
Generation National Airspace F. Brown, M. Robuck, E. Kaiser, W. J. L. Bendle, L. W. Weihmuller, Bell
Integration Ohlerking, E. Schellhase, E. Helicopter Textron Inc. and K.
W. Fulton and N. Lappos, Bell Mychalowic, D. Paul, The Boeing Clark, Magnesium Elektron
Helicopter Textron, Inc. Company
Paper #7 – 11:30 a.m. – 12 noon * Paper #7 – 11:30 a.m. – 12 noon •
High Speed Gear Windage CFD Fracture Mechanics Testing in
Analysis and Application to the Support of Bonded Joint and
NASA Glenn Gear Windage Test Composite Laminate Flaw
Facility Tolerance
M. J. Hill, R. F. Kunz, R. W. Noack, C. M. Gatley, A. S. Llanos, P. H.
L. N. Long, Pennsylvania State Jouin, The Boeing Company
University, R. F. Handschuh, NASA
Glenn Research Center
3
Technical Sessions FORUM 66
B: WEDNESDAY, MAY 12, 2010 – MORNING
Aerodynamics II Advanced Vertical Crash Safety II Flight Simulation I
8:00 a.m. – 12:15 p.m. Flight II + Unmanned 8:00 a.m. – 12:15 p.m. 8:00 a.m. – 11:45 a.m.
Room 164 VTOL AC/RC I Room 160 Room 161
Session Chair: Mahendra Bhagwat, Session Chair: David Laananen, Session Chair: Mark E. Dreier, Bell
U.S. Army AMRDEC 8:00 a.m. – 11:45 a.m. Arizona State University (Ret.) Helicopter Textron, Inc.
Room 166
Session Chairs: Michael Yu,
Continuum Dynamics, Inc. and Paper #1 – 8:00 a.m. – 8:30 a.m. (+)
Joerg Dittrich, DLR Progress in the Development of
Paper #1 – 8:00 a.m. – 8:30 a.m. Unified Fidelity Metrics for
Paper #1 – 8:00 a.m. – 8:30 a.m. Paper #1 – 8:00 a.m. – 8:30 a.m. Belt Mounted Airbag System for Rotorcraft Flight Simulators
A Variational Method for Variable Fidelity Preliminary Use in Helicopter Applications M. White, P. Perfect, G. Padfield,
Computing the Optimal Design Tools for Advanced Vertical T. Rathmann-Ramlow and J. University of Liverpool, A. W.
Aerodynamic Performance of Flight Vehicles Ksiazkiewicz, BAE Systems Gubbels, National Research
Conventional and Compound G. Whitehouse, T. R. Quackenbush, Council of Canada and A.
Helicopters and A. H. Boschitch, Continuum Berryman, Consultant Test Pilot
K. C. Hall, Duke University and S. Dynamics, Inc.
R. Hall, MIT Paper #2 – 8:30 a.m. – 9:00 a.m. Paper #2 – 8:30 a.m. – 9:00 a.m.
Technology Demonstration of a Rapid Integration, Development
Paper #2 – 8:30 a.m. – 9:00 a.m. Paper #2 – 8:30 a.m. – 9:00 a.m. Closely-Coupled Helicopter and Flight Test of Helicopter Flight
Simpilified Analysis of Sectional Behavior of an Extremely Flexible Occupant Restraint System Control Laws
Airloads on Morphing Airfoils Rotor in Hover and Forward Flight C. Culbertson, C. Van Druff, J. Shue and S. Winger, Bell
L. A. Ahaus, D. A. Peters, and A. J. J. Sicard and J. Sirohi, University of MillenWorks, B. Pilati, US Army Helicopter Textron Inc., and A. W.
Kahler, Washington University Texas at Austin AATD Gubbels and K. Ellis, National
Research Council of Canada
Paper #3 – 9:00 a.m. – 9:30 a.m. Paper #3 – 9:00 a.m. – 9:30 a.m. Paper #3 – 9:00 a.m. – 9:30 a.m.
Aerodynamic Evaluation of Simulation of Cycloidal Rotor Lightweight, High Performance Paper #3 – 9:00 a.m. – 9:30 a.m.
Miniature Trailing-Edge Effectors System using an Overset RANS Aircraft Fuel Bladders In-Flight Simulation Control Law
for Active Rotor Control Solver K. Heater, METSS Corp. and B. Design and Validation for
C. G. Matalanis, B. E. Wake, D. K. Yang, V. K. Lakshminarayan, J. Pilati, U.S. Army AATD RASCAL
Opoku, United Technologies D. Baeder, University of Maryland B. T. Fujizawa, Ames Research
Research Center, B. Y. Min, N. Center, C. M. Ivler, M. B. Tischler,
Yeshala, L. Sankar, Georgia Institute E. Moralez III, and LTC S. Braddom,
of Technology USA, U.S. Army AFDD
Refreshments Refreshments Refreshments Refreshments
9:30 a.m. – 10:15 a.m. 9:30 a.m. – 10:15 a.m. 9:30 a.m. – 10:15 a.m. 9:30 a.m. – 10:15 a.m.
Paper #4 – 10:15 a.m. – 10:45 a.m. Paper #4 – 10:15 a.m. – 10:45 a.m. (+) Paper #4 – 10:15 a.m. – 10:45 a.m. Paper #4 – 10:15 a.m. – 10:45 a.m.
The Flow Physics of Helicopter New Design of a Variable A Study of Rotary-Wing Crashes Application of Task-Pilot-Vehicle
Brownout Geometry Prop-Rotor with Cable to Support New Crashworthiness (TPV) Models in Flight Simulation
C. Phillips, H. W. Kim, R. E. Brown, and Hydraulic-System Actuation Criteria R. K. Heffley, Robert Heffley
University of Glasgow R. Turmanidze, Georgian Technical L. Labun, Safe, Inc. Engineering
University and L. Dadone, The
Boeing Company
Paper #5 – 10:45 a.m. – 11:15 a.m. Paper #5 – 10:45 a.m. – 11:15 a.m. Paper #5 – 10:45 a.m. – 11:15 a.m. Paper #5 – 10:45 a.m. – 11:15 a.m.
Mesoscale Sediment Tracking Flight Testing and Closed Loop Comparison of Heart and Aortic Modeling Lead-Lag Dynamics for
Methodology to Analyze Brownout Control of a Shrouded Rotor Micro Injuries to Head, Neck and Spine Rotorcraft-Pilot-Couplings
Cloud Developments Air Vehicle with Anti Torque Injuries in US Army Aircraft Investigation
M. Syal, B. Govindarajan, and J. G. Vanes Accidents from 1983 to 2005 M. Pavel, Delft University of
Leishman, University of Maryland V. Hrishikeshavan, and I. Chopra, T. Barth, AmSafe Aviation and P. Technology
University of Maryland Balcena, U.S. Army Aeromedical
Research Laboratory
Paper #6 – 11:15 a.m. – 11:45 a.m. Paper #6 – 11:15 a.m. – 11:45 a.m. Paper #6 – 11:15 a.m. – 11:45 a.m. Paper #6 – 11:15 a.m. – 11:45 a.m.
CFD Validation of Micro Hovering Active Control of UAV Helicopter Suggestions to Refine the UH-60MU Low Frequency Model
Rotor in Ground Effect with a Slung Load for Precision Investigation of Helicopter Correlation
T. S. Kalra, V. K. Lakshminarayan, Airborne Cargo Delivery Mishaps C. Quiding, Sikorsky Aircraft Corp.
and J. D. Baeder, University of K. Kang, J. Ottander, J. V. R. Prasad, L. Labun, Safe, Inc.
Maryland and E. Johnson, Georgia Institute
of Technology
Paper #7 – 11:45 a.m. – 12:15 p.m. (+) Paper #7 – 11:45 a.m. – 12:15 p.m.
In Ground Effect Aerodynamics of Study on Rotorcraft Safety and
Rotors with Different Blade Tips Survivability
J. Milluzzo, A. Sydney, and J. G. M. Couch, Institute for Defense
Leishman, University of Maryland Analysis and D. Lindell, Joint
Aircraft Survivability Program
Office
4
Technical Sessions FORUM 66
B: WEDNESDAY, MAY 12, 2010 – MORNING
Operations II Product Support Propulsion II Structures and
8:00 a.m. – 10:45 a.m. 8:00 a.m. – 11:45 a.m. 8:00 a.m. – 11:15 a.m. Materials II
Room 165 Room 162 Room 163 8:00 a.m. – 12:15 p.m.
Session Chair: Allen Huber, Session Chair: Ty Genteman, Session Chair: William T. Storey, Room 167
U.S. Army Aviall Services, Inc. Goodrich Engine Control Systems Session Chair: Jon Schuck, AATD
Paper #1 – 8:00 a.m. – 8:30 a.m. Paper #1 – 8:00 a.m. – 8:30 a.m.
Paper #1—8:00 a.m. – 8:30 a.m. Paper #1 – 8:00 a.m. – 8:30 a.m. Validation, Verification, and Journey to Achieve Fatigue
3D-LZ Brownout Landing Solution Airframe Condition Evaluation Hardware implementation of Reliability – From the Notional
W. Harrington, J. Savage, R. A. (ACE) & Corrosion Prevention and Physics-Based PHM Systems for Six-Nine’s Reliability Approach to
McKinley, U.S. Air Force Research Control Evaluation (CPCE) Continuous Power Assurance, Advanced Fatigue Reliability
Laboratory and LTC S. Braddom D. Duran, U.S. Army AMRDEC Erosion Detection, and Model- Methodology
and Z. Szoboszlay, U.S. Army AFDD Based Torque for Helicopter J. Zhao and D.O. Adams, Sikorsky
and H. N. Burns, H. N> Burns Turboshaft Engines Aircraft Corp.
Engineering Corp. J. Goericke, K. Moeckly, O. G.
Harris, R. Luppold, and A.
Paper #2 – 8:30 a.m. – 9:00 a.m. Paper #2 – 8:30 a.m. – 9:00 a.m. (+) Stramiello, Honeywell Aerospace
Blast Fragmentation Tolerant Army Platform Maintenance
Canopy for an AH-1W Cobra Application - A-State-of-the-Art Paper #2 – 8:30 a.m. – 9:00 a.m. Paper #2 – 8:30 a.m. – 9:00 a.m.
J. Schadler and M. Squires, Bell Solution to Process Development of a Multi-faceted Further Advances in a Recently
Helicopter Textron Inc. HUMS/Diagnostics Data Integrated Health Management Developed Cumulative-Damage
J. Magson, J. Cycon, D. Spare, System for Rotorcraft Engines Reliability Method
Sikorsky Aircraft Corp. and B. G. Gordon, A. Peralta, and R. R. E. Benton Jr., U.S. Army Aviation
Plummer, Utility Helicopter Office Patankar, Honeywell Aerospace Engineering Directorate
Paper #3 – 9:00 a.m.—9:30 a.m. Paper #3 – 9:00 a.m. – 9:30 a.m. Paper #3 – 9:00 a.m. – 9:30 a.m. Paper # 3 – 9:00 a.m. – 9:30 a.m.
Operational benefits of an Rotary Wing Structural Life Conceptual Design of a Two Spool V-22 Web Based Fatigue & Usage
Optimal, Widely Variable Speed Tracking Architecture Compressor for the NASA Large Monitoring System
Rotor D. Algera, N. Iyyer, C.-H. Hong, S. Civil Tilt Rotor Enginer S. Moon, L-3 Communications, J.
J. DiOttavio and D. Friedmann, Sarkar, A. Singh, and S. Bradfield, J. P. Veres, NASA Glenn Research Claus, C. Miller, B. Lloyd, G.
U.S. Army AATD Technical Data Analysis, Inc. Center and D. R. Thurman, U.S. Lofberg, and M. Allard, NAVAIR
Army Research Laboratory and R. Bellville, M. Stull, and S.
Kestel, L-3 Communications
Refreshments Refreshments Refreshments Refreshments
9:30 a.m. – 10:15 a.m. 9:30 a.m. – 10:10 a.m. 9:30 a.m. – 10:15 a.m. 9:30 a.m – 10:15 a.m.
Paper #4 – 10:15 – 10:45 a.m. Paper #4 – 10:15 a.m. – 10:45 a.m. Paper #4 – 10:15 a.m. – 10:45 a.m. Paper #4 – 10:15 a.m. – 10:45 a.m.
The Joint Multi-Role Aircraft RIMFIRE - A Failure Reporting Effects of Gas Turbine Component Revaluation of OH-58 Dynamic
Analysis Study: Support for Army and Corrective Action Monitoring Performance on Engine and Component Lives when
Aviation Requirements in the 2025 System Rotary Wing Vehicle Size and Incorporating a Revised Usage
Timeframe and Beyond D. Hutson, QinetiQ North America Performance Spectrum
L. Sisson, Fort Rucker, US Army C. A. Snyder, NASA Glenn Research S. M. Parker, Bell Helicopter
Center and D. R. Thurman, US Textron Inc. and J. W. Bullock, U.S.
Army Research Laboratory Army Aviation Engineering
Paper #5 – 10:45 a.m. – 11:15 a.m. Directorate
Maintenance Reduction of Paper #5 – 10:45 a.m. – 11:15 a.m. Paper #5 – 10:45 a.m. – 11:15 a.m.
Composite Main Rotor Blades: Assessment of Aerodynamic Integrated Statistical Stress Life
Graphite Trailing Edge Stiffeners Challenges of a Variable-Speed Analysis Methodology Utilizing
M. Cappelli, Sikorsky Aircraft Corp. Power Turbine for Large Civil Tilt- Local Stress Fields
Rotor Application M.R. Urban, Sikorsky Aircraft Corp.,
G.E. Welch, NASA Glenn Research G. Bauer and T. Meyer, Computer
Center Aided Engineering Associates, Inc.,
A. Ghohal and G.S. Welsh, United
Paper #6 – 11:15 a.m. – 11:45 a.m. * Technologies Research Center, and
Providing Expert Engineering N. Bordick, U.S, Army AATD
Solutions for Aviation Maintainers
Worldwide Paper #6 – 11:15 a.m. – 11:45 a.m.
R. Horn, USARDEC Implementation of Structural
Health Monitoring for the USMC
CH-53E
J. Thomas and C. Neubert, NAVAIR,
M. D. Little, In Service Support
Center, Cherry Point, and B. L.
Fuller, Naval Surface Warfare
Center
Paper #7 – 11:45 a.m. – 12:15 p.m.
Engineering Trade-off between
Performance Enhancement and
Weight Reduction for Gear
Housing using Mathematical
Optimization
B. Hansen, Sikorsky Aircraft Corp.
and D. Marjadi, Altair Engineering,
Inc.
5
Technical Sessions FORUM 66
C: WEDNESDAY, MAY 12, 2010 – AFTERNOON
Aerodynamics III Aircraft Design I Dynamics I Flight Simulation II
1:45 p.m. – 6:00 p.m. 1:45 p.m. – 5:30 p.m. 1:45 p.m. – 6:00 p.m. 1:45 p.m. – 6:00 p.m.
Room 164 Room 165 Room 166 Room161
Session Chair: Richard Brown, Session Chair: Martin Sekula, NASA Session Chair: Claudio Monteggia, Session Chair: Duc T. Tran, NASA
University of Glasgow Langley Research Center AgustaWestland Ames Research Center
Paper #1 – 1:45 p.m. – 2:15 p.m. Paper #1 – 1:45 p.m. – 2:15 p.m. Paper #1—1:45 – 2:15 p.m. Paper #1 – 1:45 p.m. – 2:00 p.m.
Time-refinement within a A Methodology for Rotorcraft Whirl Test of a Large Scale High Optimization of a Disturbance
Cartesian off-body grid/ Brownout Mitigation Using Rotor Authority Active Flap Rotor Rejection Compensator Using a
curvilinear near-body grid Design Optimization P. F. Lorber, J. J. O’Neill, B. Isabella, Unified Simulation and Control
L.A. Salcedo, C. Benoit, S. Péron, J. Tritschler, M. Syal, R. Celi, and J. J. Andrews, J. Wong, B. Hein, and Tool
and G. Jeanfaivre, ONERA G. Leishman, University of D. Geiger, Sikorsky Aircraft Corp. D. Lee, C. He, and J. Zhao,
Maryland and B. E. Wake, U. Jonsson, and F. Advanced Rotorcraft Technology,
Sun, United Technologies Research Inc.
Center
Paper #2 – 2:15 – 2:45 p.m. Paper #2 – 2:15 p.m. – 2:45 p.m. Paper #2 – 2:15 p.m. – 2:45 p.m. Paper #2—2:15 p.m. – 2:45 p.m.
Application and Validation of Optimal Aerodynamic Design of a A CFD-CSD Coupled-Analysis of A Networked Simulation
High-Order Unstructured Grid Coaxial Rotor System in Hover HART-II Rotor Vibration Environment for Dynamic
Schemes to Vortex-Dominant and Axial Flight Reduction using Gurney Flaps Interface Flight Control Design
Flows O. Rand and V. Khromov, B.-Y. Min, L. N. Sankar, O. A. and Evaluation
C. Sheng, Q. Zhao, The University Technion, Israel Institute of Bauchau, Georgia Institute of R. McKillip, Jr. and J. Keller,
of Toledo Technology Technology Continuum Dynamics, Inc.
Paper #3 – 2:45 p.m. – 3:15 p.m. Paper #3 – 2:45 p. m. – 3:15 p.m. Paper #3 – 2:45 p.m. – 3:15 p.m. Paper #3 – 2:45 p.m. – 3:15 p.m.
A Coupled Unstructured-Adaptive Design and Testing of a Ducted A Comprehensive Study of Active Determining the Impact of
Cartesian CFD Approach for Coaxial Rotor System for Microflaps for Vibration Reduction Hangar-Edge Modifications on
Hover Prediction Application to a Micro Aerial in Rotorcraft Ship-Helicopter Operations using
A. Wissink, M. Potsdam, V. Vehicle A, K. Padthe, L. Liu, and P. P. Offline and Piloted Helicopter
Sankaran, U.S. Army AFDD amd J. T. E. Lee, J. G. Leishman, University Friedmann, University of Michigan Flight Simulation
Sitaraman, Z. Yang, and D. of Maryland and O. Rand, J. Forrest, C. H. Kääriä, and I.
Mavriplis, University of Wyoming Technion, Israel Institute of Owens, University of Liverpool
Technology
Refreshments Refreshments Refreshments Refreshments
3:15 p.m. – 4:00 p.m. 3:15 p.m. – 4:00 p.m. 3:15 p.m. – 4:00 p.m. 3:15 p.m. – 4:00 p.m.
Paper #4 – 4:00 p.m. – 4:30 p.m. Paper #4 – 4:00 p.m. – 4:30 p.m. Paper #4 – 4:00 p.m. – 4:30 p.m. Paper #4 – 4:00 p.m. – 4:30 p.m.
An Analysis of Grid Reduction for Bell 429 Main Rotor Aerodynamic Investigation of Rotor Performance Extracting Airwake Cross-
Solving Rotor Blade with and Dynamic Development and Loads of a UH-60A Correlation and Cross-Spectrum
CFD/Doublet Surface/Free Wake J. C. Narramore, M. Yuce, B. J. Individual Blade Control System Models from a Database for
Coupling Thomas, Bell Helicopter Textron H. Yeo, U.S. Army AFDD and E. A. Routine Applications
S. Y. Wie, J. S. Jang, D. J. Lee, KAIST Inc. Romander and T. R. Norman, G. H. Gaonkar and R. Mohan,
NASA Ames Research Center Florida Atlantic University
Paper #5 – 4:30 p.m. – 5:00 p.m. Paper #5 – 4:30 p.m. – 5:00 p.m. Paper #5 – 4:30 p.m. – 5:00 p.m. Paper #5 – 4:30 p.m. – 5:00 p.m.
Investigation of Mixed Element Performance Improvement with Comprehensive UH-60 Loads Enhanced Numerical Simulations
Hybrid Grid-Based CFD Methods Variable Rotor Span and RPM Model Validation of Helicopter Landing Maneuvers
for Rotorcraft Flow Analysis M. Mistry and F. Gandhi, The C. McColl and D. Palmer, Technical in Brownout Conditions
G. R. Whitehouse and A. H. Pennsylvania State University Data Analysis, Inc. and M. A. D'Andrea and F. Scorcelletti,
Boschitsch, Continuum Dynamics, Chierichetti, O. Bauchau, M. and AgustaWestland
Inc., M. Smith, C. E. Lynch, Ruzzene, Georgia Institute of
Georgia Institute of Technology, Technology
and R. E. Brown, University of
Glasgow.
Paper #6 – 5:00 p.m. – 5:30 p.m. Paper #6 – 5:00 p.m. – 5:30 p.m. • Paper #6 – 5:00 p.m. – 5:30 p.m. Paper #6 – 5:00 p.m. – 5:30 p.m. (+)
A Rotorcraft Aerodynamics CFD Reverse Engineering in the Dynamic Analysis and Mathematical Modeling of the
Solution Method Based on Helicopter Performance Optimization of a Smart Flapping NOTAR Anti-Torque System for
Vorticity Confinement Evaluation Wing Flight Simulation
Y. Wenren and S. Chitta, Flow F. D. Grande, F. Scorcelletti, M. S. Mukherjee and R. Ganguli, I. Yavrucuk, H. M. Bakir, and O.
Analysis, Inc., D. A. Wachspress, Cicale, AgustaWestland Indian Institute of Science Uzol, Middle East Technical
Continuum Dynamics, Inc., and J. University
Steinhoff, U. of TN Space Inst.
Paper #7—5:30 p.m. – 6:00 p.m. Paper #7—5:30 p.m. – 6:00 p.m. Paper #7 – 5:30 p.m. – 6:00 p.m.
Physical and Numerical Issues in Load Reduction in Lead-Lag Hardware-in-the-Loop
the Prediction of Free Wake Hover Dampers by Speed-Scheduled Development Simulator to support
Performance Aperture and Modulated Control the CH-53G Avionics Upgrade
S. Schmitz, University of California, of a By-Pass Valve Development and Certification
Davis, M. J. Bhagwat, F. X. C. L. Bottasso, S. Cacciola, A. Croce, J. Otte, J. Müeller, A. Pebler,
Caradonna, U.S. Army (AMRDEC) L. Dozio, Politecnico di Milano Eurocopter Deutschland GmbH
6
Technical Sessions FORUM 66
C: WEDNESDAY, MAY 12, 2010 – AFTERNOON
HUMS I Propulsion III Structures & Materials III Unmanned VTOL AC/RC II
1:45 p.m. – 5:30 p.m. 1:45 p.m. – 5:30 p.m. 1:45 p.m. – 6:00 p.m. 1:45 – 5:3 0 p.m.
Room 160 Room 163 Room 167 Room 162
Session Chair: Edwin Martin, U.S. Session Chair: William Storey, Session Chair: Clyde Simmerman, Session Chair: Joerg Dittrich, DLR
Army AMRDEC Goodrich Engine Control Systems Naval Air System Command
Paper #1 – 1:45 p.m. – 2:15 p.m. Paper #1 – 1:45 p.m. – 2:15 p.m. Paper #1 – 1:45 p.m. – 2:15 p.m. Paper #1 – 1:45 p.m. – 2:15 p.m.
A Systematic Approach to Bearing Extension-Twist Coupled Analysis of Interlaminar Damages Autorotation Path Planning using
Health Monitoring Graphite/Epoxy Composite in Thick Rotorcraft Composite Reachable Sets and Optimal
O. Uluyol, K. Kim, C. Driveshafts for Gear-Mesh Components by Embedded Sensors Control
Hickenbottom, Honeywell Vibration Suppression S. L. Butler, A. Ghoshal, M. R. S. Tierney and J. Langelaan, The
Aerospace H. DeSmidt and J. Zhao, University Gurvich, G. S. Welsh, United Pennsylvania State University
of Tennessee Technologies Research Center, M.
R. Urban, Sikorsky Aircraft Corp.,
Paper #2 – 2:15 p.m. – 2:45 p.m. and N. Bordick, U.S. Army AATD
Paper #2 – 2:15 – 2:45 p.m. An Approach to Fault Diagnosis
Gear Fault Location Detection for and Failure Prognosis of Spline Paper #2 – 2:15 p.m. – 2:45 p.m. Paper #2 2:15 p.m. – 2:45 p.m.
Split Torque Gearbox using AE Wear Application of Shape Memory Autonomous Autorotation Flights
Sensors J. Goldsmith, R. Ehinger, and C. E. Alloy Hybrid Composites for of Helicopter UAVs to Known
R. Li, D. He, University of Illinois at Covington, Bell Helicopter Textron Variable-Twist Proprotors Landing Sites
Chicago and E. Bechhoefer, Inc., D. Edwards, T. Khawaja, C. J.-S. Park, S.-H. Kim, and S. N. Jung, J. Holsten, S. Loechelt, and W.
Goodrich Sensors and Integrated Sconyers, Z. Voulgaries,, and G. Konkuk University Alles, Aachen University
Systems Vachtsevanos, Georgia Institute of
Technology,
Paper #3 – 2:45 p.m. – 3:15 p.m.
Evaluation of Gear Condition Paper #3 – 2:45 p.m. – 3:15 p.m. Paper #3 – 2:45 p.m. – 3:15 p.m. Paper #3 – 2:45 p.m. – 3:15 p.m. *
Indicator Performance on Design and Test of the Kamatics Quasi-Static and Cyclic Apprenticeship Learning for
Rotorcraft Fleet Tufflex Tail Rotor DriveShaft Interlaminar Cracking Behavior of Autonomous Helicopter Aerobatics
L. J. Antolick and J. S. Branning, Coupling Glass Fiber/MWCNT/Epoxy and Auto-Rotation Landings
RMCI, Inc., D. R. Wade, U.S. Army R. T. Ehinger and D. Mueller, Bell Hybrid Composites P. Abbeel, UC Berkley, A. Coates,
Aviation Engineering Directorate, Helicopter Textron Inc., and J. Y. Zhu and C. E. Bakis, The and A.Y. Ng, Stanford University
and P. J. Dempsey, NASA Glenn Unghire, J. Parekh, W. Muskus Pennsylvania State University
Research Center Kamatics Corp.
Refreshments Refreshments Refreshments Refreshments
3:15 p.m. – 4:00 p.m. 3:15 p.m. – 4:00 p.m. 3:15 p.m. – 4:00 p.m. 3:15 p.m. – 4:00 p.m.
Paper #4 – 4:00 p.m. – 4:30 p.m. Paper #4 – 4:00 p.m. – 4:30 p.m. Paper #4 – 4:00 p.m. – 4:30 p.m. Paper #4 – 4:00 p.m. – 4:30 p.m.
Correlate Life Predictions and Implications of Simultaneous Robert L. Lichten Winner: The ONERA ReSSAC Unmanned
Condition Indicators in Helicopter Mechanical and Thermal Loads Next Generation Graphene Autonomous Helicopter: Visual
Tail Gearbox Bearings on the Rheological Properties of Nanocomposites for Rotorcraft Air-to-Ground Target Tracking in
P. J. Dempsey, NASA Glenn the Grease in AH-64 Helicopter Structural Applications an Urban Environment
Research Center, N. Bolander, and Gearboxes M. A. Rafiee, Rensselaer Polytechnic Y. Watanabe, C. Lesire, A.
C. Hayes, Sentient Corp., J. P. Nooli, A. Bayoumi, N. Goodman, Institute Piquereau, P. Fabiani, M.
Branning, RMCI, Inc., and D. R. V. Blechertas, F. Gadala-Maria, N. Sanfourche, and G. Le Besnerais,
Wade - U.S. Army Aviation Goodman, and V. Blechertas, ONERA
Engineering Directorate University of South Carolina
Paper #5 – 4:30 p.m. – 5:00 p.m. Paper #5 – 4:30 p.m. – 5:00 p.m. Paper #5 – 4:30 p.m. – 5:00 p.m. Paper #5 – 4:30 p.m. – 5:00 p.m.
A Control Theory Approach to An Integrated, Real-time Oil Fatigue Damage Simulations in Benchmarking of Obstacle Field
Machinery Health Prognostics Quality Monitor and Debris Composites Navigation Algorithms for
E. Bechhoefer, Goodrich SIS and Measurement Capability for Drive Y. Nikishkov and A. Makeev, Autonomous Helicopters
D. He, The University of Illinois at train and Engine Systems Georgia Institute of Technology B. Mettler and Z. Kong, University
Chicago C. Byington, C. A. Palmer, G. of Minneapolis, C. Goerzen, Ames
Argenna, and N. Mackos, Impact Research Center, and M. Whalley,
Technologies, LLC, R. Moss, A. U.S. Army AFDD
Paper #6 – 5:00 p.m. – 5:30 p.m. Toms, and K. Goddard, GasTOPS, Paper #6 – 5:00 p.m. – 5:30 p.m.
Comparison of Test Stand and Inc., and J. Moffat, U.S. Army Structural Integrity of Composite Paper #6 – 5:00 p.m. – 5:30 p.m.
Helicopter Oil Cooler Bearing RDECOM/AATD Rotor Blades with Service and Motion Planning for an
Condition Indicators Ballistic Damages Autonomous Helicopter in a GPS-
P. J. Dempsey, NASA Glenn Paper #6 – 5:00 p.m. – 5:30 p.m. R. S. Kumar and M. R. Gurvich, denied Environment
Research Center, J. Branning, Development of Corrosion Sensor United Technologies Research S. Potyagaylo, O. Rand, and Y.
RCMI, Inc., D. R. Wade, U.S. Army Technology for Rotorcraft Center, M.R. Urban and M.D. Kanza, Technion, Technion -- Israel
Aviation Engineering Directorate, G. M. Light, G. Vasquez, Jr., T. S. Cappelli, Sikorsky Aircraft Corp. Institute of Technology
and N. Bolander, Sentient Mintz, C. E. Duffer, A. C. Cobb,
Corporation Southwest Research Institute, M.
McGlaun and R. T. Ehinger, Bell
Helicopter Textron Inc., and J. Paper #7 – 5:30 p.m. – 6:00 p.m. •
Fetty, U.S. Army AATD Simulation, Tracking, and
Comparing Multiple-Mode
Progressive Failure Events in
Composite Structures
L. W. Bark and M. Macias, MSC
Software Corporation
7
Technical Sessions FORUM 66
D: THURSDAY, MAY 13, 2010 – MORNING
Aerodynamics IV + Aircraft Design II Avionics I Crew Stations and Dynamics II
Acoustics I 8:00 a.m. – 11:45 a.m. 8:00 a.m. – 12:15 p.m. Human Factors 8:00 a.m. – 11:45 a.m.
8:00 a.m. – 11:45 a.m. Room 165 Room 163 8:00 a.m. – 11:15 a.m. Room 166
Room 164 Session Chair: Richard Session Chair: Ryland Room 156 Session Chair: Askari Badre-
Session Chairs: Marty Markiewicz, DSTL Barlow, U.S. Army TAPO Session Chair: Roy Wagner, Alam, LORD Corporation
Moulton, U. S. Army, AED Lockheed Martin
and Juliet Page, Wyle Paper #1 – 8:00 – 8:30 a.m.
Laboratories, Inc. Development of an Active Paper #1 – 8:00 \– 8:30 a.m. Paper #1 – 8:00 – 8:30 a.m. (+) Paper #1 – 8:00 – 8:30 a.m.
Trim Tab System for Development of an Forward-Looking Integrated Investigation of Helicopter
Paper #1 – 8:00 – 8:30 a.m. Onboard Rotor Tracking Augmented Visionics System Symbology for 4-D Seat Structural Dynamics
Validations of Coupled CSD C. G. Matalanis, A. Kuczek, R- to Aid Flight Operations in ReRoutable Helicopter for Aircrew Vibration
/ CFD and Particle Vortex S. Lin, E. Manies. B. E. Wake Degraded Visual Approach-to-Landing Mitigation
Transport Method for and, J. Yeh, United Environments E. Moralez III and R. J. Y. Chen, V. Wickramasinghe,
Rotorcraft Applications: Technologies Research N. Link and D. Brown, CAE, Shively, U.S. Army AFDD A. Corbin, D. Zimcik,
Hover, Transition, and High Center, and Z. Chaudhry and Inc., E. Trickey, Neptec (AMRDEC), A. J. Grunwald, National Research Council
Speed Flights P. Brewer, Hamilton Design Group, and S. Technion, Israel Institute of Canada
P. Anusonti-Inthra, National Sundstrand Jennings, National Research Technology and Lt. Col. M.
Institute of Aerospace Council of Canada Hovev, Israeli Air Force
Paper #2 – 8:30 – 9:00 a.m. Paper #2 – 8:30 – 9:00 a.m.
Paper #2 – 8:30 – 9:00 a.m. On Power and Actuation Paper # 2 – 8:30 – 9:00 a.m. Paper #2 – 8:30 – 9:00 a.m. Vibration Analysis and
Coupled CFD-Simulation of Requirement in ALLFlight - A Synthetic Visual-Vestibular Feedback Testing of Bell 429
a Helicopter in Free Flight Swashplateless Primary Vision Sensor Suite with for Enhanced Situational Helicopter
Trim Control using Trailing-Edge ‘See-Through’ Capability for Awareness in Teleoperation K. Riedel, Bell Helicopter
M. Embacher, M. Keßler, E. Flaps Helicopter Applications of UAVs Textron Inc.
Krämer, Universität Stuttgart, C. Duling and F. Gandhi, The T. Lueken and H.-U. Doehler, P. R. Giordano, H. Deusch, J.
M. Dietz, Eurocopter Pennsylvania State University German Aerospace Center Lächele, and H. H. Bülthoff,
Deutschland GmbH and F. Straub, The Boeing Max Planck Institute for
Company Biological Cybernetics Paper #3 – 9:00 – 9:30 a.m.
Paper #3 – 9:00 – 9:30 a.m. Paper #3 – 9:00 – 9:30 a.m. Implementation of DYMORE
Multidisciplinary CFD/CSD Paper #3 – 9:00 – 9:30 a.m. Remote Guardian System Paper #3 – 9:00 – 9:30 a.m. (CSD) / Overflow -2 (CFD)
Analysis of the Smart Active Development of an SNU (RGS) Defensive Weapon Alternative Human Machine Loose Coupling Methodology
Flap Rotor Intelligent Rotor Blade with System Interface Display Concepts at BHTI
M. Potsdam and M. V. an Active Trailing-edge Flap C. Weaver, BAE Systems for Next Generation Military J. A. Morillo, M. Summers,
Fulton, U.S. Army AFDD J. Lee, J. Kwak, K. Son, and S. Rotorcraft and J. O. Bridgeman, Bell
(AMRDEC) and A. Dimanlig, Sin, Seoul National R. A. Faerber, The Boeing Helicopter Textron Inc.
ELORET Corp. University Company
Refreshments Refreshments Refreshments Refreshments Refreshments
9:30 a.m. – 10:15 a.m. 9:30 a.m. – 10:15 a.m. 9:30 a.m. – 10:15 a.m. 9:30 a.m. – 10:15 a.m. 9:30 a.m. – 10:15 a.m.
Paper #4 – 10:15 – 10:45 a.m. Paper #4 – 10:15 – 10:45 a.m. Paper #4 – 10:15 – 10:45 a.m. Paper #4 – 10:15 – 10:45 a.m. Paper #4 – 10:15 – 10:45 a.m.
Aeromechanic and Cheeseman Award Paper: Effective Collision Avoidance Landing an H-60 in Brown- Rotor Vibration Reduction
Aeroacoustic Predictions of High-Fidelity Optimization Systems for Light Helicopters Out Conditions Using 3D-LZ using an Embedded
the Boeing SMART Rotor Framework for Helicopter R. F. Healing, R Cubed Displays Spanwise Absorber
Using Coupled CFD/CSD Rotors Consulting Z. Szoboszlay and S. J. Austruy, F. Gandhi - The
Analysis M. Imiela, DLR Braddom, U. S. Army AFDD, Pennsylvania State
J. Bain, Georgia Institute of Paper#5 – 10:45 – 11:15 a.m. H. N. Burns, H. N. Burns University, and N. Lieven,
Technology, M. Potsdam, U.S. Reusable Automated Engineering Corp., R. A. The University of Bristol
Army AFDD, L. Sankar, Platform SIL Testing - A McKinley, W. Harrington,
Georgia Institute of Cost-Effective Risk-Reduced and J. C. Savage, Air Force
Technology, and K. S. Process for Airworthy Research Laboratory
Brentner, The Pennsylvania Reusable Software
State University S. Simi, S. Koester, R. Zepeda,
Tucson Embedded Systems,
Paper #5 – 10:45 – 11:15 a.m. Paper #5 – 10:45 – 11:15 a.m. Inc. and S. Tompkins, U. S. Paper #5 – 10:45 – 11:15 a.m. Paper #5 – 10:45 – 11:15 a.m.
Prediction and Validation of Development of a Army SED — Airworthiness Brownout Landing Aid A Multibody Formulation
the Aerodynamics, Framework for Optimizing Simulation Technology for Three Dimensional Brick
Structural Dynamics and Aspects of Rotor Blades Paper #6 – 11:15 –11:45 a.m. (BLAST) Finite Element Based
Acoustics of the SMART C. S. Johnson, G. Barakos, Brownout Cloud T. S. Turpin, Turpin Parallel and Scalable Rotor
Rotor Using a Loosely- University of Liverpool Characterization Using the Technologies, B. Sykora, BAE Dynamic Analysis
Coupled CFD-CSD Analysis Modulation Transfer Systems, G. Neiswander, San A. Datta, ELORET Corp., W.
S. Ananthan and J. D. Baeder, Function (+) Jose State University, and Z. Johnson, NASA Ames
University of Maryland, B. J. Tritschler and R. Celi, Szoboszlay, U.S. Army AFDD Research Center
W-C. Sim, UARC/AFDD, S. University of Maryland
Hahn and G. Iaccarino,
Stanford University Paper #7 – 11:45 – 12:15 a.m.
Automatic Recovery of Paper #6 – 11:15 – 11:45 a.m.
Paper #6 – 11:15 – 11:45 a.m. Paper #6 – 11:15 – 11:45 a.m. Helicopter to Level Flight Prediction and Fundamental
Direct CFD Predictions of Aerodynamic Design from Difficult Attitude Using Understanding of Stall
Low Frequency Sounds Optimization of Helicopter Adaptive Flight Control Loads in UH-60A Pull-up
Generated by a Helicopter Rotor Blades including System Based on Neural Maneuver
Main Rotor Airfoil Shape Network and Fuzzy Expert A. Abhishek, S. Ananthan, J.
B. W. Sim, UARC/AFDD, M. N. A. Vu, J.-W. Lee, Y.-H. System • Baeder, and I. Chopra,
Potsdam, US Army AFDD, D. Byun, and S.-H. Kim, Konkuk A. A. Orlov, M. V. Pavlenko, University of Maryland
Conner, US Army University G. V.Liseykin, A. K.
AFDD/JRPO, and M. E. Watts, Samorukov, V. N. Grigoriev,
NASA Langley Research A. V. Mesyanzhin,
Center Innovation Engineering
Center
8
Technical Sessions FORUM 66
D: THURSDAY, MAY 13, 2010 – MORNING
Handling Qualites I HUMS II HUMS II Systems Test and
8:00 a.m. – 12:15 p.m. 8:00 a.m. – 12:15 p.m. Continued Engineering I Evaluation I
Room 161 Room 160 8:00 a.m. – 11:45 a.m. 8:00 a.m. – 12:15 p.m.
Session Chair: David Miller, Session Chair: Michael J. Room 167 Room 162
Boeing Rotorcraft Systems Augustin, Bell Helicopter Session Chair: Michael Session Chair: Ronald
Textron Inc. Gaydar, NAVAIR Walden, NAVAIR
Paper #1 – 8:00 – 8:30 a.m.
The State-Space Free-Vortex Paper #7 – 11:45 –12:15 p.m.
Paper #1 – 8:00 – 8:30 a.m. Paper #1 – 8:00 – 8:30 a.m. Paper #1 – 8:00 – 8:30 a.m.
Wake: A Control-Oriented Aircraft Health
Asymmetric Acoustic Airworthiness Integration The Experimental
Model Management Technology
Scattering for Structural into Modern Systems Investigation of a Rotor
P. Betoney, R. Celi, and J. G. Deployment via IVHMU
Health Monitoring Engineering for Complex Hover Icing Model with
Leishman, University of Third-Party Software
S. Costiner, H. Winston, A. Military Aircraft Systems Shedding
Maryland Capability *
Ghoshal, G. S. Welsh, and E. D. P. Schrage, Georgia E. W. Brouwers, J. L. Palacios,
J. Isom, M. Davis, Sikorsky
Paper #2 – 8:30 – 9:00 a.m. N. Manes, United Institute of Technology and E. C. Smith, The
Aircraft Corp. and L. LaPierre,
Simulation of Coaxial- Technologies Research Pennsylvania State University
GE Aviation
Helicopter UAV’s Flight Test Center, M. R. Urban and M. Paper #2 – 8:30 – 9:00 a.m. and A. A. Peterson, Boeing
Program based on ADS-33E- Davis, Sikorsky Aircraft Corp. Multi-Variable Analysis in Rotorcraft
PRF for Control System and N. Bordick, U. S. Army Design Requirements
Performance Evaluation Aviation Applied Technology Development Paper #2 – 8:30 – 9:00 a.m.
S. Loechelt and W. Alles, Directorate J. Lloyd and A. Weick, Bell An Evaluation of Anti-icing
Aachen University and F. Helicopter Textron Inc. Test Results for the AH-64D
Linke, German Aerospace Paper #2 – 8:30 – 9:00 a.m. Block III Engine Nose
Center (DLR) Self-Powered Helicopter Gearbox Fairing
Health Monitoring Sensor L. Buck, The Boeing
Paper #3 – 9:00 – 9:30 a.m. D. Berdy, S. Scott, J. Jang, D. Company and B. Dodson,
Development and Adams, B. Jung, F. Sadeghi, Goodrich Corp.
Evaluation of Reduced Order and D. Peroulis, Purdue
Models of On-Blade Control University Paper #3 – 9:00 – 9:30 a.m. Paper #3 – 9:00 – 9:30 a.m.
for Integrated Flight and Quantitative Risk Photogrammetric
Rotor Control Paper # 3 – 9:00 – 9:30 a.m. Assessment – An Application Measurements of an EH-60L
F. E. Olcer, J. V. R. Prasad, L. Energy Harvesting and of Life Data Analysis Brownout Cloud
N. Sankar, and J. J. Bain, Embedded RF Wireless L. Pham, P. Hensley, Sikorsky O.D. Wong and P.E. Tanner,
Georgia Institute of Sensor Systems for Helicopter Aircraft Corp. US Army AFDD/JRPO
Technology and J. Zhao and Blades
C. He, Advanced Rotorcraft A. Fang, M. Bryant, E. Garcia,
Technology, Inc. Cornell University
Refreshments Refreshments Refreshments Refreshments
9:30 a.m. – 10:15 a.m. 9:30 a.m. – 10:15 a.m. 9:30 a.m. – 10:15 a.m. 9:30 a.m. – 10:15 a.m.
Paper #4 – 10:15 – 10:45 a.m. Paper #4 – 10:15 – 10:45 a.m. Paper #4 – 10:15 – 10:45 a.m. Paper #4 – 10:15 – 10:45 a.m.
An Investigation of Large Smart Embedded Sensors in A Conversation on Systems Icing Trial for Qualification
Tilt-Rotor Short-term Rotorcraft Composite Engineering Attributes of the New AW101 Main
Attitude Response Handling Components for Condition M. Gaydar, NAVAIR and Tail Rotors Utilizing the
Qualities Requirements in Based Maintenance (+) Helicopter Icing Spray
Hover A. Ghoshal, G. S. Welsh, M. Paper #5 – 10:45 – 11:15 a.m. System (HISS)
C. A. Malpica, W. A. Decker, R. Gurvich, S. L. Butler, H. A Survey of Agile Methods, T. Neville and K. Robinson,
and C. R. Theodore, NASA Winston, S. Costiner and P. Processes and Tools AgustaWestland
Ames Research Center and C. Attridge, United Technologies D. Sabados, P. Componation,
Blanken, U.S. Army AFDD Research Center, M. R. and S. O’Brien, University of Paper #5 – 10:45 – 11:15 a.m.
(AMRDEC), and T. Berger, Urban, Sikorsky Aircraft Alabama in Huntsville, F. Adverse Environment Rotor
University of California, Corp., and N. Bordick, U.S. Shull, Fraunhofer Center for Test Stand Calibration
Santa Cruz Army AATD Experimental Software Procedures and Ice Shape
Engineering, R. Turner, Correlation
Paper #5 – 10:45 – 11:15 a.m. Paper #5 – 10:45 – 11:15 a.m. Stevens Institute of J. L. Palacios, E. W.
Determining Effects of Time- Magnetoelastic Torque Technology and E. Colbert, Brouwers,Y. Han and E. C.
Varying Rotorcraft Dynamics Sensor Systems for Helicopter University of Southern Smith, The Pennsylvania
on Pilot Control Powertrain HUMS and California. State University
T. K. Nicoll and D. G. Control Applications (+)
Mitchell, Hoh Aeronautics, R. J. Kari, M. Hollander, and
Inc. I. J. Garshelis, MagCanica, Paper #6 – 11:15 – 11:45 a.m. Paper #6 – 11:15 – 11:45 a.m.
Inc.and M. W. Davis, Sikorsky Enterprise Systems Shore Based Hover Trials
Paper #6 – 11:15 – 11:45 a.m. Aircraft Corp. and K. A. Engineering: Advanced using a Helmet Mounted
Use of Wavelet Scalograms Calhoun, Rolls-Royce Digital Collaboration Tools Display
to Characterize Rotorcraft and Methodology for J. van der Vorst and A. de
Pilot-Vehicle System Paper #6 – 11:15 – 11 45 a.m. Improved Product Reus, NLR
Interactions Rotary Wing Dynamic Integration
D. H. Klyde, P. C. Schulze, C. Component Structural Life T. Saunders, L. Levine, D.
Y. Liang, P. M. Thompson, Tracking with Self-Powered Cocuzzo, R. Bourque, and B.
Systems Technology, Inc. Wireless Sensors (+) Brooks, Sikorsky Aircraft
J. Loverich, J. Frank, KCF Corp. Paper #7 – 11:45 – 12:15 p.m.
Paper #7 – 11:45 – 12: 15 p.m. Technologies, Inc., E. C. Initial Power-off Testing of
Use of Rotor State Feedback Smith, The Pennsylvania the BA609 Tiltrotor (+)
to Improve Closed Loop State University, and J. Szefi, J.C. Harris, P. Scheidler, R.
Stability and Handling Invercon, LLC Hopkins, and R.
Qualities Fortenbaugh, Bell Helicopter
J. F. Horn, W. Guo, and G. T. (See next Column) Textron Inc.
Ozdemir, The Pennsylvania
State University
9
Technical Sessions FORUM 66
E: THURSDAY, MAY 13, 2010 – AFTERNOON
Acoustics II Aircraft Design III Avionics II Dynamics III
1:30 p.m. – 5:00 p.m. 1:30 p.m. – 5:00 p.m. 1:30 p.m. – 3:30 p.m. 1:30 p.m. – 5:00 p.m.
Room 164 Room 165 Room 163 Room 166
Session Chair: Juliet Page, Wyle Session Chair: Martin Sekula, Session Chair: Allen Walker, U.S. Session Chair: Lau Benton, NASA
Laboratories, Inc. NASA Langley Research Center Army AATD Ames Research Center
Paper #1 – 1:30 p.m. – 2:00 p.m. Paper #1 – 1:30 p.m. – 2:00 p.m. Paper #1 – 1:30 p.m. – 2:00 p.m. Paper #1 – 1:30 p.m. – 2:00 p.m.
Long-Range and Nonlinear Undergraduate 26th Annual Apache Block III Participation in Stochastic Aeroelastic Analysis of
Propagation of Helicopter High- AHS/Industry Student Design the On-The-Move Field Exercise Articulated Helicopter Rotor using
Speed Impulsive Noise Competition Winner K. Wroblewski, M. E. Palich, and W. Response Surface
S. Lee, K. S. Brentner, and P. J. Presentation R. Levin, The Boeing Company Approximations
Morris, The Pennsylvania State Gyr Blitz by P. Gore, T. Keister and P. Beena and R. Ganguli, Indian
University C. Brown, Georgia Institute of Institute of Science
Technology
Paper #2 – 2:00 p.m. – 2:30 p.m. Paper #2 – 2:00 p.m. – 2:30 p.m.
Paper #2 – 2:00 p.m. – 2:30 p.m. Paper #2 – 2:00 p.m. – 2:30 p.m. MH-60 Link-16 Integration Unified Assessment of Fast-
A Parameter Identification Graduate 26th Annual P. Stiles and J. Hess, Lockheed Floquet, Generalized-Floquet and
Method for Helicopter Noise AHS/Industry Student Design Martin Mission Systems & Sensors Periodic-Eigenvector Methods for
Source Identification and Physics- Competition Winner and J. Turner, NAVAIR Rotorcraft Stability Predictions
Based Semi-Empirical Modeling Presentation R. Mohan and G. H. Gaonkar,
E. Greenwood, NASA Langley Peregrine by A. Robledo, S. Ashok, Florida Atlantic University
Research Center and F. H. Schmitz, and M. Osman, Georgia Institute of
University of Maryland Technology
Paper #3 – 2:30 p.m. – 3:00 p.m. Paper #3 – 2:30 p.m. – 3:00 p.m.
Paper #3 – 2:30 p.m. – 3:00 p.m. Paper #3 – 2:30 p.m. – 3:00 p.m. (+) Development of a Robust, Helicopter Landing Gear Shimmy
Validation of EC130 and EC145 Performance Metrics for Assessing Segmented Approach to UAV Analysis
Environmental Impact Assessment Potential of Advanced Rotorcraft Handover in the Overarching D. Butts and A. Kogan, Sikorsky
Using HELENA Concepts Interoperability Profile for Class C Aircraft Corp.
M. Gervais, V. Gareton, A. J. D. Sinsay, U.S. Army AMRDEC CUCS
Dummel, and R. Heger, Eurocopter C. Li, The Boeing Company and S.
F. Gilpin, Air Axis, LLC
Refreshments Refreshments Refreshments Refreshments
3:00 p.m. – 3:30 p.m. 3:00 p.m. – 3:30 p.m. 3:00 p.m. – 3:30 p.m. 3:00 p.m. – 3:30 p.m.
Paper#4 – 3:30 – 4:00 p.m. Paper #4 – 3:30 p.m. – 4:00 p.m. Paper #4 – 3:30 p.m. – 4:00 p.m. Paper #4 – 3:30 p.m. – 4:00 p.m.
A Computational Study of BVI Development and Flight Networking Challenges for Aeroservoelastic Analysis of
Noise Reduction Using Active Validation of an Autonomous Rotorcraft Rotorcraft-Pilot Coupling: a
Twist Control Mono-Wing UAS T. A. DuBois, W. B. Blanton, K. Parametric Study
D. E. Fogarty, National Institute of K. Fregene, S. Jameson, and D. Wroblewski, and J. Clemens, The P. Masarati, Politecnico de Milano
Aerospace, M. L. Wilbur, U. S. Army Sharp, Lockheed Martin Advanced Boeing Company and M. Gennaretti, Universit•
Research Laboratory, and M. K. Technology Laboratories, H. Roma
Sekula, NASA Langley Research Youngren, AeroCraft Consulting,
Center and D. Stuart, Dave Stuart Model
Aircraft
Paper #5 – 4:00 p.m. – 4:30 p.m. (+)
Paper #5 – 4:00 – 4:30 p.m. Paper #5 – 4:00 p.m. – 4:30 p.m. Using Tightly-Coupled CFD/CSD
On-Blade Harmonic Acoustic The S-61: The Next 50 Years Simulation for Rotorcraft Stability
Control to Minimize Near In-Plane H. C. Curtiss, Princeton University Analysis
Far-Field Helicopter Rotor Noise and F. Carson, Carson Helicopters, A. Zaki, N. Reveles, M. J. Smith,
G. Gopalan, C. Sargent, and F. H. Inc. and O. A. Bauchau, Georgia
Schmitz, University of Maryland Institute of Technology
Paper #6 – 4:30 p.m. – 5:00 p.m. • Paper #6 – 4:30 p.m. – 5:00 p.m. (+) Paper #6 – 4:30 p.m. – 5:00 p.m.
Numerical Investigation of VABS-IDE: VABS-Enabled Application of CFD/CSD to Rotor
Fuselage Shielding Effects on Rotor Integrated Design Environment Aeroelastic Stability in Forward
Noise (IDE) for Efficient High-Fidelity Flight
S. Mählmann, DLR Composite Rotor Blade and Wing H. Yeo, M. Potsdam, and R. A.
Design Ormiston, U.S. Army AFDD
P. Hu, Advanced Dynamics (AMRDEC)
Corporation, W. Yu, Utah State
University, D. Hodges, George
Institute of Technology, and J. Ku,
Independent Contractor
10
Technical Sessions FORUM 66
E: THURSDAY, MAY 13, 2010 – AFTERNOON
Handling Qualites II HUMS III Systems Engineering II Test and Evaluation II
1:30 p.m. –4:30 p.m. 1:30 p.m. – 5:30 p.m. 1:30 p.m. – 5:00 p.m. 1:30 p.m. – 5:00 p.m.
Room 161 Room 160 Room 167 Room 162
Session Chair: Paul Schifferle, Session Chair: Paula Dempsey, Session Chair: Steve Skinner, Bell Session Chair: Oliver Wong,
Calspan Corp. NASA Glenn Research Center Helicopter Textron Inc. AFDD/JRPO
Paper #1 – 1:30 p.m. – 2:00 p.m. Paper #1 – 1:30 p.m. – 2:00 p.m. Paper #1 – 1:30 p.m. – 2:00 p.m. Paper #1 – 1:30 p.m. – 2:00 p.m.
Development of External Load Development of an Airframe UAS Deployed Live Training: Determination of Shipborne
Handling Qualities Criteria for Intensity Based Structural Health Perception or Reality? Helicopter Launch and Recovery
Rotorcraft Monitoring System D. Ratliff, US Army, PEO STRI, O. S. Limitations using Computational
J. Lusardi, C. L. Blanken, S. R. S. C. Conlon, M. R. Shepherd, J. A. Fedak, The Boeing Co. and D. Geis, Fluid Dynamics
Braddom, U.S. Army AFDD Hines, A. R. Barnard, F. Semperlotti, US Army FFID M.R. Snyder, J.S. Burks, C. J.
(AMRDEC) P. Q. Romano, E. C. Smith, The Brownell, L. Luznik, D. S.
Pennsylvania State University Paper #2 – 2:00 p.m. – 2:30 p.m. Miklosovie, J. H. Golden, M. E.
Multistate Wind Computation: Hartsog, G. E. Lemaster, F. D.
Paper #2 – 2:00 p.m. – 2:30 p.m. Paper #2 – 2:00 p.m. – 2:30 p.m. Use of Aircraft Accelerations to Robertson, J. P. Shishkoff, and W. P.
CH-53K Control Laws: An Composite Damage Detection in Selectively Use Conventional Wind Stillman, U.S. Naval Academy
Overview and some Analytical Aircraft Structures Using Triangle and Cycloid
Results Vibration Measurements of Computations to Improve Paper #2 – 2:00 p.m. – 2:30 p.m.
V. Sahasrabudhe, A. Faynberg, S. Modulation Under Operational Accuracy of the Cockpit Wind In-Flight and Ground
Kubikl, O. Tonello and H. Xin, Loading Display Instrumentations for Dauphin’s
Sikorsky Aircraft Corp. and D. B. Zwink, N. Yoder, D. Adams, D. A. F. Schaefer, J. J. Saunders, and M. FENESTRON Noise Investigation
Engel and J. Renfrow, NAVAIR Koester, Purdue University and C. S. Randolph, Lockheed Martin L. Binet, F. Cuzieux, ONERA and
Jones, U.SMC, and M. Yu, U. S. J.C. Camus and L. Perthuis, CEV
Paper #3 – 2:30 p.m. – 3:00 p.m. Navy Paper #3 – 2:30 p.m. – 3:00 p.m..
U. S. Army Airworthiness Achieving Safe and Effective UAS Paper #3 – 2 :30 p.m. – 3 :00 p.m.
Approval for UH-60 Fly-By-Wire Paper #3 – 2:30 p.m. – 3:00 p.m. Control for the U.S. Army’s Bi- Whirl Testing of a Pneumatic
Aircraft Flight Testing Advanced CBM Technologies for Directional Remote Video Artificial Muscle Actuation System
F. Luria and T. Vongpaseuth, US Helicopter Rotor Systems - Full Terminal for a Full-Scale Active Rotor
Army Aviation Engineering Scale Rotor Demonstration and D. Limbaugh, Kutta Technologies, B.K.S. Woods, N.M. Wereley,
Directorate and J. W. Harding, Test Results Inc., R. Higgins, U.S. Army AATD, University of Maryland and C.S.
Harding Consulting, Inc. J. R. Andrews and M. Augustin, Bell P. Cates, U.S. Army Unmanned Kothera, Techno-Sciences, Inc.
Helicopter Textron Inc. Aircraft Systems Project Oiice, and
L. Ericsson, U.S. Army, Redstone
Arsenal
Refreshments Refreshments Refreshments Refreshments
3:00 p.m. – 3:30 p.m. 3:00 p.m. – 3:30 p.m. 3:00 p.m. – 3:30 p.m. 3:00 p.m. – 3:30 p.m.
Paper #4 – 3:30 p.m. – 4:00 p.m. Paper #4 – 3:30 p.m. – 4:00 p.m. (+) Paper #4 – 3 :30 – 4:00 p.m. Paper #4 – 3:30 p.m. – 4:00 p.m.
Flight Testing of Load Alleviating Rotorcraft Dynamic Component On the Business Impact of Quality Experimental Investigation of an
Control and Tactile Cueing System Usage Based Maintenance Process Management Avian-Based Flapping Wing
O Wulff, V. Sahasrabudhe, R. Beale, P. R. Bates, M. Davis, and P. Sadegh, M. S. Cohen and J. Chard, IBM Concept in Hover and Forward
R. Lamb, and J. Rigsby, Sikorsky Sikorsky Aircraft Corp. Flight for Micro Air Vehicle
Aircraft Corp. and J. W. Fletcher, Applications
and S. Braddom, U.S. Army AFDD R. Malhan, M. Benedict, and I.
(AMRDEC) Chopra, University of Maryland
Paper #5 – 4:00 p.m. – 4:30 p.m. Paper #5 – 4:00 p.m. – 4:30 p.m. Paper #5 – 4:00 p.m. – 4:30 p.m. Paper #5 – 4:00 p.m. – 4:30 p.m. (+)
Bell 429 Handling Qualities and Fault Class Identification through Rational Harmony for Systems MV-22B Osprey Deck Heating
AFCS Flight Test Results and Pilot Applied Data Mining of AH-64 Engineering - Best Practices for Effects on Navy Amphibious
Evaluations Condition Indicators Model-based Systems Engineering Assault Ships
J. Schillings, C. Griffith, E. N. Goodman and A. Bayoumi, H.-P. Hoffman, IBM E. S. Alley, Naval Surface Warfare
Oltheten, E. Emblin, and E. University of South Carolina Center and V. T. Mitchell, Naval Air
Lambert, Bell Helicopter Textron Warfare Center Aircraft Div.
Inc. and J. Dionne, Bell Helicopter
Textron Canada, Ltd. Paper #6 – 4:30 p.m. – 5:00 p.m. Paper #6 – 4:30 p.m. – 5:00 p.m.
Calculating Fatigue Damage with Organizing Systems Engineering
Wireless Sensors: Duty Cycling vs. Plans with Users in Mind
Down Sampling S. K. O’Brien, L. H. Liever, and D.
S. W. Arms, J. Martin, C. P. M. Sabados, University of Alabama
Townsend, D. L. Churchill, in Huntsville
MicroStrain, Inc. and D.
Liebschutz and N. Phan, NAVAIR
Paper #7 – 5:00 p.m. – 5:30 p.m.
Usage Based Fatigue Damage
Calculation for AH-64 Apache
Dynamic Components
P. Shanthakumaran, T. Larchuk, R.
Christ, D. Mittleider, and E.
Hitchcock, The Boeing Company
11
Plan now to attend
AHS International
67th Annual Forum
& Technology Display
May 3-5, 2011 •Virginia Beach Convention Center •Virginia Beach, VA
12
