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UW Wing Design.xls - UW Departments Web Server Powered By Docstoc
					Subsonic Transport Composite Wing Model
Reference: Albers, R. G., Tuttle, M. E., and Avery, W. B., "Subsonic Transport Composite Wing Model for Optimization Stud

Airfoil
Reference: Selig, M., UIUC Airfoil Coordinates Database, Version 2.0 , URL http://www.ae.uiuc.edu/m-selig/ads/coord_datab
% Upper is the percent of the airfoil that lies above the neutral line, i.e., y = 0
Difference is the normalized airfoil thickness at each chord station
% Lower is the percent of the airfoil that lies below the neutral line, i.e., y = 0

Thickness
Reference: Niu, M. C.-Y., Airframe Structural Design: Practical Design Information and Data on Aircraft Structures , Conmilit P
WBL Model is the spanwise position
Upper Model is the waterline (z) position of the upper surface of the wing
Lower Model is the waterline (z) position of the lower surface of the wing
Thickness Model is the wing thickness of the wing
Thickness T/C Ratio is the thickness-to-chord ratio of the wing

Geometry
Keypoints that define ribs are listed here in the following order: upper surface, leading edge; lower surface, leading edge; low

Wing Weight-Preliminary Design
Reference: Torenbeek, E., “Development and Application of a Comprehensive, Design-Sensitive Weight Prediction Method fo
Reference: Roskam, J., Airplane Design, Part 6: Preliminary Calculation of Aerodynamic, Thrust, and Power Characteristics , R

Aerodynamic Loads
Reference: Garcelon, J. H., Balabanov V. O., and Sobieski J., “Multidisciplinary Optimization of a Transport Aircraft Wing Using

Material Properties
Reference: Swanson, S. R., and Qian Y., “Multiaxial Characterization of T800/3900-2 Carbon/Epoxy Composites”, Composites
Reference: Mabson, G. E., and Graesser D. L., “Cost Optimization Software for Transport Aircraft Design Evaluation (COSTADE
Reference: Composite Materials Handbook, Vol. 2F: Polymer Matrix Composites Materials Properties , “Section 4.2.33: T700

Laminate Design
Reference: Nelson, W. D., Bunin B. L., and Hart-Smith L. J., “Critical Joints in Large Composite Aircraft Structure”, NASA, Repo

Stringer Panel
Reference: Tuttle, M. E., Structural Analysis of Polymeric Composite Materials , Marcel Dekker, Inc., New York, NY, 2004

Applied Aero Loads
Chord No., Line No., and Normalized Initial Nodal Forces are taken directly from the Aero Loads worksheet
Applied Forces and Applied Moments represent the point loads reacted at the structural box from the leading and trailing edg
KP/HP are the Keypoint and Hardpoint numbers associated with the finite element model where the applied forces and mom
Element and Element Area are the specific elements in the finite element model where the surface pressures are applied on t
Applied Tip Nodal Loads are the aerodynamic loads reacted at the tip of the wing structural box, and are listed from the leadi
Applied Tip Nodal Loads with Mass (3.75G) and (-1.5G) are the aerodynamic and mass loads reacted at the tip of the wing str

Applied Mass Loads
Reference: Torenbeek, E., Synthesis of Subsonic Airplane Design: An Introduction to the Preliminary Design of Subsonic Gene
Reference: Roskam, J., Airplane Design, Part 5: Component Weight Estimation , Roskam Aviation and Engineering Corp., Otta
Reference: Federal Aviation Administration, “Pratt & Whitney Models PW 4062 Type Certificate Data Sheet,” FAA, Report TC
Reference: General Electric Aviation, Model CF6-80C2 Engine Overview, URL http://www.geae.com/engines/commercial/cf6
Reference: Jenkinson, L. R., Simpkin P., and Rhodes D., Civil Jet Aircraft Design , AIAA, Reston, VA, 1999
For LE and TE Mass Loads, node numbers are listed as the lower surface and upper surface
For TE Mass Loads, the first mass and force numbers are for the inner 2/3 of the mass, the second, the outer 1/3 of the mass
Note that the Tip Mass Loads are included on the Applied Aero Loads worksheet and are listed as upper leading, lower leadin
For LG Mass Loads the nodes are listed as inboard upper and lower and outboard upper and lower
For Engine Mass Loads the nodes are listed as trailing to leading edges

Applied Fuel Pressures
Reference: Coordinating Research Council, Inc., Handbook of Aviation Fuel Properties , Society of Automotive Engineers, Inc.,
Volume ID is the same as bay number, i.e., volume 1 is contained by ribs 1 & 2
Cell Lower Area and Fuel Load, along with bay volume, is used to calculate the Total Pressure in a given fuel bay
Height is the inboard TE line or smallest inboard line height, and is used to calculate the shared rib net pressure
KP is the keypoint at which the Z Coordinate is defined; this is used in ANSYS to define the linear variation of the presssure on

Emergency Landing Loads
Reference: Niu, M. C.-Y., Airframe Stress Analysis and Sizing , Conmilit Press Ltd., Hong Kong, 1997
Reference: Howe, D., Aircraft Loading and Structural Layout , AIAA, Reston, VA, 2004
Wing Model for Optimization Studies", Proceedings of the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference , V


 iuc.edu/m-selig/ads/coord_database.html - B, Nov. 11, 2005 [cited March 13, 2006]




a on Aircraft Structures , Conmilit Press Ltd., Hong Kong, 1988




e; lower surface, leading edge; lower surface, trailing edge; and upper surface, trailing edge


 itive Weight Prediction Method for Wing Structures for Transport Category Aircraft”, Delft University of Technology, Report LR-693, Delft
 rust, and Power Characteristics , Roskam Aviation and Engineering Corp., Ottawa, KS, 1990


 of a Transport Aircraft Wing Using VisualDOC”, Proceedings of the 40th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and


n/Epoxy Composites”, Composites Science and Technology , Vol. 43, No. 2, 1992, pp. 197-203
rcraft Design Evaluation (COSTADE)--User's Manual”, NASA Langley Research Center, Report NASA CR-4738, Hampton, VA, Aug., 1996
 Properties , “Section 4.2.33: T700S 12k/3900-2 Plain Weave Fabric”, and “Section 4.2.34: T800HB 12k/3900-2 Unidirectional Tape”, U.S.


 e Aircraft Structure”, NASA, Report NASA CR 3710, Washington, DC, Aug., 1983


ker, Inc., New York, NY, 2004


oads worksheet
 x from the leading and trailing edges
where the applied forces and moments are applied
 surface pressures are applied on the lower wing surface
 box, and are listed from the leading to trailing edges
  reacted at the tip of the wing structural box
eliminary Design of Subsonic General Aviation and Transport Aircraft, with Emphasis on Layout, Aerodynamic Design, Propulsion, and Perfo
 iation and Engineering Corp., Ottawa, KS, 1989
 icate Data Sheet,” FAA, Report TCDS No. E24NE, Washington, DC, Apr. 19, 2002
 eae.com/engines/commercial/cf6/cf6-80c2.html [cited Mar. 27, 2006]
  n, VA, 1999

 econd, the outer 1/3 of the mass
ted as upper leading, lower leading, upper trailing, and lower trailing edges




ety of Automotive Engineers, Inc., CRC Report No. 530, Warrendale, PA, 1983

e in a given fuel bay
red rib net pressure
near variation of the presssure on the ribs and spars
s and Optimization Conference , Victoria, British Columbia, Canada, AIAA, Reston, VA, September 10-12, 2008, AIAA-2008-6016




 Technology, Report LR-693, Delft, The Netherlands, Sep., 1992




uctures, Structural Dynamics, and Materials Conference, St. Louis, MO, AIAA, Reston, VA, Apr. 12-15, 1999, pp. 1306-1313




738, Hampton, VA, Aug., 1996
3900-2 Unidirectional Tape”, U.S. Department of Defense, MIL-HDBK-17-2F, Washington, DC, June 17, 2002, pp. 4-243--4-254
amic Design, Propulsion, and Performance , Delft University Press, Delft, The Netherlands, 1982
2, 2008, AIAA-2008-6016




99, pp. 1306-1313




002, pp. 4-243--4-254
Boeing BACXXX Airfoil

          X             Y                                  0.3
Upper               0            0    % Upper Difference
Surface       0.0005        0.0037     0.672727   0.0055
               0.001         0.005     0.649351   0.0077
              0.0025        0.0078     0.644628   0.0121   0.2
               0.005        0.0112     0.658824    0.017
               0.015        0.0207     0.678689   0.0305
                 0.02       0.0242     0.683616   0.0354
               0.025        0.0271     0.684343   0.0396   0.1
              0.0375        0.0334     0.687243   0.0486
                 0.05       0.0384     0.686941   0.0559
               0.075        0.0465     0.682819   0.0681
                                                               0
                  0.1       0.0521     0.672258   0.0775
                                                                   0         0.1         0.2
               0.125        0.0566     0.662763   0.0854
                 0.15       0.0599     0.651795   0.0919
                  0.2       0.0643     0.631631   0.1018   -0.1
                 0.25       0.0665     0.614603   0.1082
                  0.3       0.0674     0.602324   0.1119
                 0.35       0.0673     0.595049   0.1131
                  0.4       0.0667     0.593416   0.1124   -0.2
                 0.45       0.0654     0.596171   0.1097
                  0.5       0.0636     0.603989   0.1053
                 0.55       0.0613     0.615462   0.0996
                  0.6       0.0585     0.629709   0.0929   -0.3
                 0.65       0.0548     0.643948   0.0851
                  0.7       0.0503      0.65924   0.0763
                 0.75        0.045     0.673653   0.0668
                  0.8       0.0384     0.688172   0.0558
                 0.85       0.0307     0.699317   0.0439
                  0.9       0.0218     0.707792   0.0308
                 0.95       0.0116     0.711656   0.0163
                    1       0.0004           0.5  0.0008

Lower               0             0   % Lower
Surface       0.0005        -0.0018    0.327273       1
               0.001        -0.0027    0.350649       1
              0.0025        -0.0043    0.355372       1
               0.005        -0.0058    0.341176       1
               0.015        -0.0098    0.321311       1
                 0.02       -0.0112    0.316384       1
               0.025        -0.0125    0.315657       1    0           0.1         0.2         0.3
              0.0375        -0.0152    0.312757       1
                 0.05       -0.0175    0.313059       1
               0.075        -0.0216    0.317181       1
                  0.1       -0.0254    0.327742       1
0.125    -0.0288   0.337237    1
 0.15     -0.032   0.348205    1
   0.2   -0.0375   0.368369    1
 0.25    -0.0417   0.385397    1
   0.3   -0.0445   0.397676    1
 0.35    -0.0458   0.404951    1
   0.4   -0.0457   0.406584    1
 0.45    -0.0443   0.403829    1
   0.5   -0.0417   0.396011    1
 0.55    -0.0383   0.384538    1
   0.6   -0.0344   0.370291    1
 0.65    -0.0303   0.356052    1
   0.7    -0.026    0.34076    1
 0.75    -0.0218   0.326347    1
   0.8   -0.0174   0.311828    1
 0.85    -0.0132   0.300683    1
   0.9    -0.009   0.292208    1
 0.95    -0.0047   0.288344    1
     1   -0.0004         0.5   1
                    y = -4.5841x6 + 15.483x5 - 20.573x4 + 13.558x3 - 4.7301x2 + 0.8405x + 0.0057
                                                     R² = 0.9933




                                                                                              Series1
                                                                                              Series2
      0.3         0.4             0.5           0.6           0.7           0.8          0.9                1
                                                                                              Poly. (Series1)
                                                                                              Poly. (Series2)

                        y = 1.9658x6 - 5.8973x5 + 6.6877x4 - 3.7444x3 + 1.3244x2 - 0.3328x - 0.0032
                                                       R² = 0.9951




0.3         0.4                0.5           0.6            0.7           0.8           0.9                1
1
WBL Model (m) Upper Model (m) Lower Model (m) Thickness Model (m)    Thickness T/C Ratio
               0    0.71558463   -0.817376808         1.532961438             1.532961438
     2.4304625      0.71558463   -0.817376808         1.532961438             1.532961438
      3.057525    0.654092854    -0.690536999         1.344629853             1.463712413
        3.72745   0.603711297    -0.625910716         1.229622013             1.392100378
      4.397375    0.561679724    -0.571995265         1.133674988             1.321783631
         5.0673   0.525619892    -0.525739988           1.05135988            1.252623699
      5.737225    0.494044094    -0.485236545         0.979280639             1.184656111
        6.40715   0.465959479    -0.449211372         0.915170851             1.117846076
      7.077075    0.440670327    -0.416772044         0.857442371             1.052227645
           7.747  0.417670168      -0.38726889        0.804939058               0.99673918
      8.512175    0.393717188    -0.356543518         0.750260706             0.934128408
        9.27735   0.371827437    -0.328464727         0.700292164               0.88601358
     9.8218625    0.357323482    -0.309859967         0.667183449             0.854401582
    10.3647875    0.343641258    -0.292309274         0.635950531             0.823259215
        10.9093   0.330620744    -0.275607379         0.606228123             0.792521583
    11.4538125    0.318234552    -0.259719154         0.577953705             0.764393697
    11.9967375    0.306457386    -0.244612149         0.551069535               0.73238886
      12.54125    0.295169397    -0.230132628         0.525302026             0.702963463
     13.084175    0.284392094    -0.216308183         0.500700277             0.674003414
    13.6286875    0.274023403      -0.20300788        0.477031283             0.645452057
        14.1732   0.264060968    -0.190228698         0.454289666             0.617338562
     14.716125    0.254501584    -0.177966522         0.432468106             0.589688253
    15.2606375      0.24526211   -0.166114708         0.411376817             0.562449116
    15.8035625    0.236372141    -0.154711216         0.391083357             0.535671726
     16.348075    0.227757788    -0.143661268         0.371419056             0.509306947
    16.8925875    0.219425709    -0.132973402         0.352399111               0.48337941
    17.4355125    0.211381142      -0.12265434        0.334035482             0.457912056
     17.980025    0.203560821    -0.112622925         0.316183746             0.433589461
      18.52295    0.195995629    -0.102918774         0.298914403             0.412405266
    19.0674625    0.188627835    -0.093467832         0.282095666             0.391703313
    19.3278125    0.185179076    -0.089043982         0.274223057               0.38184329
      19.58975    0.181755855    -0.084652889         0.266408744             0.372054454
     20.170775    0.174323097    -0.075118617         0.249441713             0.350556528
    20.7533875    0.167081978    -0.065830166         0.232912143             0.329460839
    21.3344125    0.160060273    -0.056823166         0.216883439             0.308790056
    21.9154375    0.153227253    -0.048058199         0.201285452             0.288532561
      22.49805    0.146555097    -0.039499578         0.186054675             0.268678998
     23.079075    0.140071026      -0.03118222        0.171253246             0.249462918
Rib
  1
  2
  3
  4
  7
                                         Waterline vs. Span for the Wing Model Upper and Lower
  8                                                               Surfaces
  9                           0.8
 10
 11
                              0.6
 12
 13
 14                           0.4
 15
 16                           0.2
      Waterline Station (m)




 17
 18
                                0
 19
                                     0          5         10                   15   20   25
 20
 21                           -0.2
 22
 23                           -0.4
 24
 25                           -0.6
 26
 27
                              -0.8
 28
 29
 30                            -1
                                                               Semi-Span (m)
 31
 32
 33
 34
 35
 36
 37
 38
 39
 40
pper and Lower




      25    Upper Model (m)
            Lower Model (m)
Structure Geometry                                    Wing Panel Stringers
    Rib     Keypoints   X (m)      Y (m)     Z (m) Stringer Spacing                   0.205 m
         1         14       2.43      1.98     -0.649                        8.070866142 in
                   17       2.43      1.98      0.472    Panel No.        No. of Stringers
                   16       2.43      6.84      0.378         1                  21
                   15       2.43      6.84     -0.537         2                  21
         2          1       1.63      1.98     -0.649         3                  21
                    2       1.63      1.98      0.472         4                  6
                    3       1.63      6.84      0.378         5                  12
                    4       1.63      6.84     -0.537         6                  20
         3          5       0.80      1.98     -0.649         7                  19
                    6       0.80      1.98      0.472         8                  18
                    7       0.80      6.84      0.378         9                  18
                    8       0.80      6.84     -0.537        10                  17
         4        146       0.00      1.98     -0.649        11                  17
                  147       0.00      1.98      0.472        12                  16
                  148       0.00      6.84      0.378        13                  15
                   13       0.00      6.84     -0.537        14                  15
         5        158      -0.74      2.48     -0.659        15                  14
                  155      -0.74      2.46      0.488        16                  14
                  156       0.00      3.60      0.558        17                  13
                  157       0.00      3.62     -0.683        18                  13
         6        154      -1.48      2.97     -0.667        19                  12
                  151      -1.48      2.95      0.504        20                  12
                  152       0.00      5.22      0.506        21                  11
                  153       0.00      5.24     -0.639        22                  11
         7        149      -2.22      3.43     -0.674        23                  10
                  150      -2.22      3.43      0.474        24                  10
                  148       0.00      6.84      0.378        25                  9
                   13       0.00      6.84     -0.537        26                  9
         8        145      -2.80      3.80     -0.663        27                  8
                  142      -2.80      3.80      0.428        28                  8
                  143      -0.64      7.14      0.279        29                  7
                  144      -0.64      7.14     -0.523        30                  7
         9        141      -3.36      4.17     -0.646        31                  6
                  138      -3.36      4.17      0.417        32                  6
                  139      -1.24      7.42      0.272        33                  6
                  140      -1.24      7.42     -0.510        34                  5
        10        137      -3.91      4.53     -0.629        35                  5
                  134      -3.91      4.53      0.406        36                  4
                  135      -1.85      7.71      0.265        37                  4
                  136      -1.85      7.71     -0.497        38                  3
        11        133      -4.47      4.89     -0.612        39                  3
                  130      -4.47      4.89      0.395
                  131      -2.46      7.99      0.258
                  132      -2.46      7.99     -0.483
        12        129      -5.03      5.25     -0.595
     126    -5.03    5.25    0.385
     127    -3.06    8.27    0.251
     128    -3.06    8.27   -0.470
13   125    -5.75    5.72   -0.573
     122    -5.75    5.72    0.370
     123    -3.85    8.64    0.242
     124    -3.85    8.64   -0.453
14   121    -6.48    6.19   -0.551
     118    -6.48    6.19    0.356
     119    -4.64    9.01    0.232
     120    -4.64    9.01   -0.436
15   117    -6.99    6.52   -0.535
     114    -6.99    6.52    0.346
     115    -5.21    9.27    0.226
     116    -5.21    9.27   -0.424
16   113    -7.50    6.86   -0.520
     110    -7.50    6.86    0.336
     111    -5.77    9.53    0.219
     112    -5.77    9.53   -0.412
17   109    -8.02    7.19   -0.504
     106    -8.02    7.19    0.326
     107    -6.33    9.80    0.213
     108    -6.33    9.80   -0.400
18   105    -8.54    7.53   -0.488
     102    -8.54    7.53    0.316
     103    -6.89   10.10    0.207
     104    -6.89   10.10   -0.387
19   101    -9.05    7.86   -0.473
      98    -9.05    7.86    0.305
      99    -7.45   10.30    0.200
     100    -7.45   10.30   -0.375
20    97    -9.56    8.20   -0.457
      94    -9.56    8.20    0.295
      95    -8.02   10.60    0.194
      96    -8.02   10.60   -0.363
21    93   -10.10    8.53   -0.441
      90   -10.10    8.53    0.285
      91    -8.58   10.80    0.187
      92    -8.58   10.80   -0.351
22    89   -10.60    8.86   -0.426
      86   -10.60    8.86    0.275
      87    -9.14   11.10    0.181
      88    -9.14   11.10   -0.339
23    85   -11.10    9.20   -0.410
      82   -11.10    9.20    0.265
      83    -9.70   11.40    0.174
      84    -9.70   11.40   -0.327
24   81   -11.60    9.53   -0.394
     78   -11.60    9.53    0.255
     79   -10.30   11.60    0.168
     80   -10.30   11.60   -0.314
25   77   -12.10    9.87   -0.379
     74   -12.10    9.87    0.245
     75   -10.80   11.90    0.161
     76   -10.80   11.90   -0.302
26   73   -12.70   10.20   -0.363
     70   -12.70   10.20    0.235
     71   -11.40   12.20    0.155
     72   -11.40   12.20   -0.290
27   69   -13.20   10.50   -0.347
     66   -13.20   10.50    0.224
     67   -11.90   12.40    0.148
     68   -11.90   12.40   -0.278
28   65   -13.70   10.90   -0.332
     62   -13.70   10.90    0.214
     63   -12.50   12.70    0.142
     64   -12.50   12.70   -0.266
29   61   -14.20   11.20   -0.316
     58   -14.20   11.20    0.204
     59   -13.10   12.90    0.135
     60   -13.10   12.90   -0.254
30   57   -14.70   11.50   -0.300
     54   -14.70   11.50    0.194
     55   -13.60   13.20    0.129
     56   -13.60   13.20   -0.241
31   53   -15.20   11.90   -0.285
     50   -15.20   11.90    0.184
     51   -14.20   13.50    0.122
     52   -14.20   13.50   -0.229
32   49   -15.70   12.20   -0.269
     46   -15.70   12.20    0.174
     47   -14.80   13.70    0.116
     48   -14.80   13.70   -0.217
33   45   -16.00   12.40   -0.262
     42   -16.00   12.40    0.169
     43   -15.00   13.80    0.113
     44   -15.00   13.80   -0.211
34   41   -16.20   12.50   -0.254
     38   -16.20   12.50    0.164
     39   -15.30   14.00    0.110
     40   -15.30   14.00   -0.205
35   37   -16.80   12.90   -0.237
     34   -16.80   12.90    0.153
     35   -15.90   14.30    0.103
            36   -15.90   14.30   -0.192
      36    33   -17.30   13.20   -0.221
            30   -17.30   13.20    0.143
            31   -16.50   14.50    0.096
            32   -16.50   14.50   -0.179
      37    29   -17.90   13.60   -0.204
            26   -17.90   13.60    0.132
            27   -17.10   14.80    0.089
            28   -17.10   14.80   -0.166
      38    25   -18.40   14.00   -0.187
            22   -18.40   14.00    0.121
            23   -17.70   15.10    0.082
            24   -17.70   15.10   -0.153
      39    21   -19.00   14.30   -0.170
            18   -19.00   14.30    0.110
            19   -18.30   15.40    0.075
            20   -18.30   15.40   -0.140
      40    10   -19.50   14.70   -0.154
            11   -19.50   14.70    0.099
            12   -18.90   15.70    0.068
             9   -18.90   15.70   -0.127
Tip        166   -18.20   12.80    0.000
           170   -18.20   13.70    0.000
           171   -18.20   14.60    0.000
           180   -18.20   15.40    0.000
           188   -18.20   16.20    0.000
ANSYS Model Areas
Upper Skin          Lower Skin            Front Spar            Rear Spar             Ribs
Panel No.   Area    Panel No.    Area     Panel No.    Area     Panel No.    Area        No.
        1        40         1         1            1      118            1      157             1
        2        41         2         2            2      119            2      158             2
        3        48         3       193            3      120            3      159             3
        4         6         4         4            4      121            4      160             4
        5         7         5         5            5      122            5      161             5
        6        43         6        82            6      123            6      162             6
        7        42         7        44            7      124            7      163             7
        8        83         8         8            8      125            8      164             8
        9        84         9         9            9      126            9      165             9
       10        88        10        10           10      127          10       166            10
       11        89        11        11           11      128          11       167            11
       12        90        12        12           12      129          12       168            12
       13        91        13        13           13      130          13       169            13
       14        92        14        14           14      131          14       170            14
       15        93        15        15           15      132          15       171            15
       16        94        16        16           16      133          16       172            16
       17        95        17        17           17      134          17       173            17
       18        96        18        18           18      135          18       174            18
       19        97        19        19           19      136          19       175            19
       20        98        20        20           20      137          20       176            20
       21        99        21        21           21      138          21       177            21
       22      100         22        22           22      139          22       178            22
       23      101         23        23           23      140          23       179            23
       24      102         24        24           24      141          24       180            24
       25      103         25        25           25      142          25       181            25
       26      104         26        26           26      143          26       182            26
       27      105         27        27           27      144          27       183            27
       28      106         28        28           28      145          28       184            28
       29      107         29        29           29      146          29       185            29
       30      108         30        30           30      147          30       186            30
       31      109         31        31           31      148          31       187            31
       32      110         32        32           32      149          32       188            32
       33      111         33        33           33      150          33       189            33
       34      112         34        34           34      151          34       190            34
       35      113         35        35           35      152          35       191            35
       36      114         36        36           36      153          36       192            36
       37      115         37        37           37      154                                  37
       38      116         38        38           38      155                                  38
       39      117         39        39           39      156                                  39
                                                                                               40
Area
       49
       45
       46
       48
       87
       86
       85
       81
       80
       79
       78
       77
       76
       75
       74
       73
       72
       71
       70
       69
       68
       67
       66
       65
       64
       63
       62
       61
       60
       59
       58
       57
       56
       55
       54
       53
       52
       51
       50
       47
Model Wing Weight Prediction
Design Weights
Maximum Take-off Weight (MTOW)             1332550.74 N
Maximum Landing Weight (MLW)               1158744.96 N
Maximum Zero Fuel Weight (MZFW)            1073770.78 N

Geometry
Reference Area S                                  283.3   m^2
Span b                                             42.2   m
Mid-chord sweep angle Λ1/2                           26   °
Leading edge sweep angle Λle                         33   °
Quarter-chord sweep angle Λ1/4                     31.5   °
Root chord (y=0) cr                       11.53180505     m
Tip chord (y=b/2) ct                      2.197963411     m
Aspect ratio A                            6.286057183
Taper ratio λ                             0.190600119           0.245
Center section span bcs                       4.860925    m
Thickness/chord ratio - root t/c          0.132933347
Thickness/chord ratio - 40% span t/c      0.084799149     Rib 14
Thickness/chord ratio - 70% span t/cref   0.087786217     Rib 26
Thickness at root (y=0) tr                1.532961438     m
Thickness at y = bcs/2 (SOB) tcs          1.532961438     m
Thickness at tip tt                       0.171253246     m
Taper ratio of wing tank λbar             0.241422481
Span of fuel tank bF                      37.79582386     m
Mean geometric chord cbar                 6.713270142     m
Mean profile thickness tref                           1   m
Fixed leading edge area Sfle                     50.994   m^2
Fixed trailing edge area Stfe                  30.5964    m^2
Leading edge slat area Sslat                       28.3   m^2
Trailing edge flap area Stef                      36.88   m^2
Trailing edge spoiler area Slift                  15.83   m^2
Aileron area Sa                                    11.2   m^2
Structural wing box area                      142.8876    m^2

Design Conditions
Design cruising speed VC                       236.64     m/s
Design cruising Mach number MC                     0.8
Design dive speed VD                        333.42576     m/s
Design dive Mach number MD                     0.8624
Design dive dynamic pressure qD           68093.30168     N/m^2
Design gust speed Ude                            15.25    m/s

Calculation of Input Data
Structural span bs                        46.95180189 m
Cantilever ratio RC                                        16.32618855
Lateral position of center of pressure ηcp                 0.497307785
Lift-curve slope CLα                                       5.940598648     1/rad   Roskam
Mass parameter μ                                           37.74082928
Gust relief factor Kg                                      0.771637776
Lateral position of fuel ybar/bF/2                         0.318860141
Lateral position of fuel ybar                              6.025790862     m
Lateral position of fuel ηf/Lateral position of cp ηcp     0.574257057
Root bending moment, lift and fuel mass MBr                25916726.81     N-m
Root bending moment, gust load MBr                         9402002.695     N-m
Mass relief, fuel, bending and shear (ΔW B+S/W B+S)F      -0.013550496
Estmated wing weight 12% MTOW                              159906.0888     N
Mass relief, mass, bending and shear (ΔW B+S/W B+S)W             -0.096
Mass relief, powerplant (ΔW B+S/W B+S)P                          -0.035
Relief factor r                                            0.855449504
Mean root stress level ρg/σbarr                            8.09526E-05     1/m
Structural efficiency ηt                                             0.8
Mean root stress / shear stress σbarr/τbar                           2.4

Weight Calculations
Bending and shear material weight, 1st term, W BASIC       69059.05433     N
Rib weight, 2nd term, W BASIC                              7372.063241     N
Primary wing box weight W BASIC                           76431.117573     N
Weight correction, sheet taper & joints ΔW NOsheet         4655.428128     N       6.091011
Weight correction, SOB joint ΔW NOsob                       1332.55074     N       1.743466
Weight correction, LG attachment ΔW NOlg                    4634.97984     N       6.064258
Weight correction, engine attachment ΔW NOeng              1838.146784     N       2.404972
Total non-optimum weight correction ΔW NO                  12461.10549     N       16.30371
Weight correction, aeroelasticity ΔW ST                    19972.26556     N       26.13107
Primary Wing Structure Weight W PRIM                     108864.488627     N
Fixed leading edge structure weight W fle                   11535.2492     N
Fixed trailing edge structure weight W tfe                 6603.275735     N
Leading edge slat weight W slat = W lef                    8186.864577     N
Trailing edge flap weight W tef                            15890.57128     N
Aileron weight (inboard & outboard) W a                    2152.088553     N
Spoiler average specific weight                                    110     N/m^2
Spoiler weight W lift                                            1741.3    N
Aileron and spoiler weight W a+s                           3893.388553     N
Flap support extra rib weight                              794.5285639     N
Ailerons support extra rib weight                          430.4177106     N
Support structure/extra rib weight W misc                  1224.946275     N
Secondary Wing Structure Weight W SEC                      47334.29562     N
Wing Weight W w                                          156198.784250     N
Atmosphere
Density ρ 20000 ft.                                                         0.65283 kg/m^3
Acceleration of gravity g 20000 ft.                                            9.807 m/s^s
Density ρSL 0 ft.                                                              1.225 kg/m^3

Manoeuver Load Factor
nult                                                                           3.75

Powerplant
Nacelle & engine weight W P                                                52518.48 N
% of MTOW                                                                 7.8823985 %
Number of engines Ne                                                              2



Materials
Specific weight, aluminum                                                      28.1 N/m^3
Shear modulus, aluminum                                                    2.81E+10 Pa

Constants
Correction factor for rib weight kr                                        5.00E-01
Non-optimum extra panel thickness δNO                                        0.0005 m
Correction factor for stiffness weight penalty f(λ)                             0.05
Correction factor for fixed leading edge/slat strengthening k fle                1.4
Correction factor for fixed trailing edge/double slotted flaps Δ                  45
Correction factor for trailing edge double slotted variable flaps k tef            2
                    4.673187017 1/rad




                                          Aluminum
                                          Mass (kg)       Old Mass (kg)
1st term, W BASIC                25.640355 7031.05827
2nd term, W BASIC                1.8521073 750.5664061
                      17182.405 lbf        7781.624676
% W BASIC                                  473.9796506
% W BASIC                                        135.67
% W BASIC                                  471.8977642
% W BASIC                                   187.145875
% W BASIC                                   1268.69329
% W BASIC                                  2033.421458
                    24473.71952 lbf        11083.73942
                                            1174.42977
                                           672.2944141
                                           833.5231702         326.4168
                                           1617.854946              718
                                           219.1089954           248.52

                                           177.2856852          352.008
                                           396.3946806          600.528



                                           124.7145464
                    10641.17684 lbf        4819.211527        2245.4728
                    35114.89635 lbf        15902.95095
Composite
Mass (kg) Weight (N)




 8866.9915   87091.591
 939.54382   9228.1994
 537.83553   5282.6206
 666.81854   6549.4917
  1294.284   12712.457
  175.2872   1721.6708

 141.82855   1393.04
 317.11574 3114.7108



 99.771637 979.95702
 3855.3692 37867.436
 12722.361 124959.03
Torenbeek Transport Airfoil Pressure Distributions
Span:
Chord (LPi)                                              Normalized Pressure       Chord Length (m)
                                                     1                       1                 11.53
                                                     2                    0.95                 10.36
                                                     3                    0.85                  9.19
                                                     4                     0.8                  8.03
                                                     5                     0.7                  6.86
                                                     6                     0.6                  5.69
                                                     7                     0.5                  4.53
                                                     8                    0.15                  3.36
                                                     9                    0.05                  2.27




Chord:
Line (CPj)                                               Normalized Pressure
                                                     1                     0.4
                                                     2                       1
                                                     3                       1
                                                     4                     0.5
                                                     5                    0.25




Torenbeek Transport Airfoil Pressure Distributions
Node Number                                              Line Number               Chord Number
                                                     1                         1                      1
                                                     2                                                2
                                                     3                                                3
                                                     4                                                4
                                                     5                                                5
                                                     6                                                6
                                                     7                                                7
                                                     8                                                8
 9       9
10   2   1
11       2
12       3
13       4
14       5
15       6
16       7
17       8
18       9
19   3   1
20       2
21       3
22       4
23       5
24       6
25       7
26       8
27       9
28   4   1
29       2
30       3
31       4
32       5
33       6
34       7
35       8
36       9
37   5   1
38       2
39       3
40       4
41       5
42       6
43       7
44       8
45       9
                                                                                     Span


                               1.2
        Normalized Pressure




                                 1           1
                                                               0.95
                               0.8                                          0.85
                                                                                         0.8
                                                                                                     0.7
                               0.6

                               0.4

                               0.2

                                 0
                                         1                 2            3            4           5
                                                                                      Chord Number




                                                                                     Chord


                               1.2
        Normalized Pressure




                                 1                                              1                    1

                               0.8

                               0.6

                               0.4                   0.4

                               0.2

                                 0
                                                 1                          2                    3
                                                                                         Line Number




Node Areas (Ai,j) (m^2)                      Aero Panel #           Area (in^2)     Area (m^2)
                              8.054485826                       1      12484.478    8.054485826
                              7.629801708                       2     12488.6004    8.057145434
                              6.779118345                       3     12487.5139    8.056444468
                              5.924437796                       4     12475.7194    8.048835128
                              5.075121398                       5     11167.9546     7.20511759
                                  4.225805                      6     11168.0913    7.205205783
                              3.371124451                       7     11167.1498    7.204598365
                              2.515598066                       8     11112.5766    7.169389919
2.086070925    9   9847.3543      6.3531191
 8.05581563   10   9847.5822   6.353266132
7.630488658   11   9846.7856   6.352752198
6.779177151   12   9749.4337   6.289944646
5.914486848   13   8518.4396   5.495756492
5.065199918   14   8456.5157   5.455805669
4.225952096   15   8566.9999   5.527085655
3.371300903   16   8386.2908   5.410499373
 2.51580342   17   7214.4682   4.654486304
2.086290473   18   7214.8788   4.654751207
8.056794951   19   7255.0357   4.680658832
7.630848512   20    7023.148   4.531054164
6.778955619   21   5885.5535   3.797123696
5.922227414   22   5886.0549   3.797447179
5.079575341   23   5885.6932   3.797213825
4.232517761   24   5660.0051    3.65160889
3.371384048   25   4564.9532   2.945125207
2.515962226   26   4565.5458   2.945507528
2.086486859   27    4565.329   2.945367658
8.052639798   28   4296.8622   2.772163617
 7.61981697   29   3233.4164   2.086070925
6.754171282   30    3234.097   2.086510021
5.895070468   31   3234.0252   2.086463698
5.037324506   32   2924.1856   1.886567582
4.165133928
3.291588497
2.422640639
 1.98651564
8.048835128
7.609112524
6.729667283
5.850222009
4.970776768
4.091331527
3.211886254
2.329365599
1.886567582
            0.7
                        0.6
                                      0.5


                                                   0.15
                                                                 0.05

        5           6             7            8           9
Chord Number




            1




                                  0.5

                                                          0.25



        3                     4                       5
Line Number




            Normalized Initial Nodal Forces (N)
                                            17479.76782
                                             15730.2163
                                            12505.18092
                                            10285.72642
                                            7709.785816
                                            5502.480866
                                            3657.990961
                                            818.8990158
226.3585547
43706.63436
39329.08143
31263.22349
25671.12516
19236.78441
13756.68101
9145.456068
2047.414661
565.9559444
43711.94764
39330.93619
31262.20187
25704.72216
19291.37987
13778.05412
9145.681618
2047.543901
 566.009219
21844.70198
 19637.0387
15573.95253
12793.42534
9565.459124
6779.350249
4464.608599
985.7983981
269.4448232
10917.19045
9804.726127
 7758.72527
6348.047821
 4719.54526
3329.613151
2178.251473
473.9218933
127.9440892
Material Properties
T800HB / 3900-2 Carbon/Epoxy Unidirectional Laminate
E11              155.8 GPa     Swanson
E22                8.89 GPa    Swanson
E33                8.89 GPa    COSTADE
ν12                 0.3        Swanson
ν13                 0.3        COSTADE
ν23             0.3675         COSTADE
G12                5.14 GPa    Swanson
G13                5.14 GPa    COSTADE
G23              3.517 GPa     COSTADE
t           0.0001905 m        MIL-HDBK-17
density           1550 kg/m^3  MIL-HDBK-17

T700S / 3900-2 Carbon/Epoxy Plain Weave Laminate       MIL-HDBK-17
*E11t           73.65 GPa       MIL-HDBK-17            *Knockdown facters based on material 4.2.2
*E11c           70.82 GPa       MIL-HDBK-17            4.2.35, T650-35 3K / 976 Plain Weave Fabric
*E22t           60.38 GPa       MIL-HDBK-17
*E22c           70.82 GPa       COSTADE                E11t              22
E33             10.26 GPa       COSTADE                E11c
*G12              5.52 GPa      MIL-HDBK-17            E22t              1.3
G13               3.83 GPa      COSTADE                E22c             1.38
G23               3.83 GPa      COSTADE                G12            0.745
*ν12            0.046           COSTADE                t             0.0052
ν13                0.4          COSTADE                E11t             10.4
ν23                0.4          COSTADE                E11c               10
t           0.000201 m          MIL-HDBK-17            E22t             8.83
density          1530 kg/m^3    MIL-HDBK-17            E22c             8.82
                                                       G12               0.8
Titanium 6Al4V          MIL-HDBK-5                     t             0.0069
Et             116.52   GPa
Ec             118.59   GPa                            E11t        47.27273
ν                0.31                                  E11c        96.15385
G               44.82   GPa                            E22t        679.2308
density      4428.78    kg/m^3                         E22c        639.1304
                                                       G12         107.3826
                                                       t           132.6923
wn facters based on material 4.2.29, T650-35 12K / 976 Uni Tape vs.
 0-35 3K / 976 Plain Weave Fabric

            Msi
            Msi
            Msi
            Msi
            Msi
            in
            Msi
            Msi
            Msi
            Msi
            Msi
            in

            %
            %
            %
            %
            %
            %
Composite Joint Laminate Design
Ply Thickness (m)               0.000191
Plain Weave Ply Thickness (m)   0.000201
             Orientation (°)         0° plies       45° plies   90° plies
PW                              45
       1                        45                          1
       2                         0              1
       3                         0              1
       4                       -45                          1
       5                        90                                      1
       6                       -45                          1
       7                         0              1
       8                        45                          1
       9                        45                          1
      10                         0              1
      11                         0              1
      12                       -45                          1
      13                        90                                      1
      14                       -45                          1
      15                         0              1
      16                        45                          1
      17                        45                          1
      18                         0              1
      19                         0              1
      20                       -45                          1
      21                        90                                      1
      22                       -45                          1
      23                         0              1
      24                        45                          1
      25                        45                          1
      26                         0              1
      27                         0              1
      28                       -45                          1
      29                        90                                      1
      30                       -45                          1
      31                         0              1
      32                        45                          1
      33                        45                          1
      34                         0              1
      35                         0              1
      36                       -45                          1
      37                        90                                      1
      38                       -45                          1
      39                         0              1
      40                        45                          1
      41                        45                          1
      42                         0              1
       43                          0          1
       44                        -45                     1
       45                         90                                 1
       46                        -45                     1
       47                          0          1
       48                         45                    1
       98 Count                               18      24         6
        1%                                 0.375      0.5    0.125
 0.018689 Thickness                    0.006858 0.009144 0.002286

Laminate Stacking Sequence Rules (Nelson 1983)
1.   Changes of only 45 degrees are allowed between interior plies
2.   No stacked plies except at the midplane
3.   Symmetry required
4.   37.5% 0 / 50% 45 / 12.5% 90
Equivalent I-stringer Stiffness Ply
Composite I-Beam
          bbf (m)                     bbf (in)        tbf (m)       h (m)             h (in)
                       0.0635                    2.5 0.018689               0.1016              4

            a11bf                      a11w           a11tf        d11bf              d11tf
                    7.225E-10            7.225E-10   7.23E-10      0.000025067       0.000025067

Composite Panel Stiffness                         Bay 5                         12 stringers
         tsk (m)                      tst (m)      wsk (m)         wst (m)           Ask (m^2)
               0.01868932               0.01868932 2.979029              0.2286        0.055676029

Composite I-Beam Plate Equivalent
           s (m)                  tI (m)      tsk (m)           Ebarxxex/I (Pa) Ebarxxex/sk (Pa)
                     0.205        0.086328904 0.018689             17890000000      74057431998

Density:
Prepreg Density (kg/m^3) Stringer Mass (kg) Stringer Density (kg/m^3)
                      1550      6.622186756 374.1893
    tw (m)           btf (m)            btf (in)           ttf (m)        Abf (m^2)   Aw (m^2)
     0.01868932            0.0635                  2.5      0.01868932    0.001186772 0.001899

Ebarxxex/bf (Pa) Ebarxxex/w (Pa)    Ebarxxex/tf (Pa) Ebarxxfl/bf (Pa) Ebarxxfl/tf (Pa) zb (m)
    74057431998     74057431998         74057431998     73332819771     73332819771 0.069489


  Ast (m^2)          a11sk              a11st            Ebarxxsk (Pa)   Ebarxxst (Pa)   β
   0.004272379         7.225E-10          7.225E-10        74057431998    74057431998 0.520606


    a11I            AI (m^2)          Ask (m^2)           Isk (m^4)     Ebarxxfl/sk (Pa) zb (m)
    6.47491E-10     0.017697425        0.003831311           1.1152E-07   73332819771 0.067982
Atf (m^2)       Ibf (m^4)                Itf (m^4)        Total Height (m)   Total Height (in)
0.001187            3.4544E-08                 3.4544E-08       0.13897864              5.4716

 zb (in) AEbarxx/beam (N) IEbarxx/beam (N-m^2)
  2.7358      316401384.1           761889.8832


a11sk-st
 3.76E-10 Constant cross section I stringer


 zb (in) AEbarxxbeam (N)          EIbarxxbeam (N-m^2)
2.676438      600343964.5                  390681.3388
Chord No. (Span)       Line No. (Chord)    Normalized Initial Nodal Forces (N)  Applied Forces (N)
                   1                   1                           17479.76782
                                       2                           43706.63436        61186.40218
                                       3                           43711.94764        43711.94764
                                       4                           21844.70198        32761.89243
                                       5                           10917.19045
                   2                   1                             15730.2163        15730.2163
                                       2                           39329.08143        39329.08143
                                       3                           39330.93619        39330.93619
                                       4                             19637.0387       29441.76482
                                       5                           9804.726127
                   3                   1                           12505.18092        12505.18092
                                       2                           31263.22349        31263.22349
                                       3                           31262.20187        31262.20187
                                       4                           15573.95253         23332.6778
                                       5                             7758.72527
                   4                   1                           10285.72642        10285.72642
                                       2                           25671.12516        25671.12516
                                       3                           25704.72216        25704.72216
                                       4                           12793.42534        19141.47316
                                       5                           6348.047821
                   5                   1                           7709.785816        7709.785816
                                       2                           19236.78441        19236.78441
                                       3                           19291.37987        19291.37987
                                       4                           9565.459124        14285.00438
                                       5                             4719.54526
                   6                   1                           5502.480866        5502.480866
                                       2                           13756.68101        13756.68101
                                       3                           13778.05412        13778.05412
                                       4                           6779.350249         10108.9634
                                       5                           3329.613151
                   7                   1                           3657.990961        3657.990961
                                       2                           9145.456068        9145.456068
                                       3                           9145.681618        9145.681618
                                       4                           4464.608599        6642.860072
                                       5                           2178.251473
                   8                   1                           818.8990158
                                       2                           2047.414661        2866.313677
                                       3                           2047.543901        2047.543901
                                       4                           985.7983981        1459.720291
                                       5                           473.9218933
                   9                   1                           226.3585547
                                       2                           565.9559444              170.91
                                       3                             566.009219             1105.4
                                       4                           269.4448232              479.39
                                       5                           127.9440892
Applied Tip Nodal Loads
           Node             FX (N)         FY (N)                MX (N-M)
                     9198              0               0.41933            -68.8
                     9197              0               0.41933            -68.8
                     6031       -1.3369                0.41933            -68.8
                     6099       -1.3369                      0                0
                     6100       -1.3369                      0                0
                     6101        -4.593             -1.389867         -196.367
                     6102        -4.593             -1.389867         -196.367
                     6103        -4.593             -1.389867         -196.367
                     6104           5.93                     0                0
                     6105           5.93                     0                0
                     6032           5.93            0.9705333        -109.7867
                     7197              0            0.9705333        -109.7867
                     7198              0            0.9705333        -109.7867
 Applied Moments (N-m)    KP/HP     Element   Element Area (m^2)
                               17       847
            61529.61579        17       847                         0.08134066
                      0       316       855                        0.131492351
           -52769.62743        16       863                        0.077316967
                               16       863
            23138.25242       317       986                        0.039668152
                      0       318       990                        0.048097575
                      0       319      3960                        0.067477113
           -70701.67068       320      3984                        0.057599803
                              320      3984
            17297.12971       321      3404                        0.088794123
                      0       322      3398                        0.106622506
                      0       323      3456                        0.109169418
           -48002.97498       324      3496                        0.080190269
                              324      3496
            13325.22423       325      3522                        0.082512454
                      0       326      3556                        0.083908975
                      0       327      3586                         0.08345952
           -32861.08761       328      3611                        0.073603613
                              328      3611
            9312.146823       329      3658                        0.092213192
                      0       330      3667                        0.098259432
                      0       331      3702                        0.094904571
           -19628.79238       332      3715                        0.052029771
                              332      3715
            6163.680091       333      3765                        0.083122428
                      0       334      3774                        0.093871895
                      0       335      3794                        0.094915272
           -10397.82109       336      3812                        0.094085921
                              336      3812
            3758.854018        50      3851                        0.089323838
                      0       337      3858                        0.081035673
                      0       338      3876                        0.085273392
           -4613.915481       339      3885                        0.066273215
                              339      3885
                              340      3930
            773.6848849       340      3930                        0.081180141
                      0       341      3936                        0.129908557
           -419.0059835       342      3941                        0.082046947
                              342      3941
                              340      3930
NA                            340      3930                        0.081180141
NA                            343      3948                         0.11890761
NA                             12      3949                        0.055759178
                               12      3949
                                 Applied Tip Nodal Loads with Mass (3.75G)
MY (N-m)           MZ (N-m)                          Node
               0       0.94124                                            9198
               0       0.94124                                            9197
       -214.5033       0.94124                                            6031
       -214.5033       0.94124                                            6099
       -214.5033       0.94124                                            6100
        -612.733       5.60933                                            6101
        -612.733       5.60633                                            6102
        -612.733       5.60633                                            6103
        -389.433      -1.90056                                            6104
        -389.433      -1.90056                                            6105
        -389.433      -1.90056                                            6032
               0   -1.9705333                                             7197
               0      -1.90056                                            7198
Applied Surface Pressure (Pa)

                  752224.0667
                  332429.5842
                  423734.8348

                  396545.2223
                  817693.6529
                  582878.1744
                  511143.4977

                  140833.4304
                  293214.1129
                  286364.0981
                  290966.4477

                  124656.6545
                  305940.1603
                  307990.2961
                  260061.5981

                  83608.27437
                  195775.4492
                  203271.3457
                  274554.4348

                   66197.3065
                  146547.3885
                  145161.6139
                  107443.9545

                  40952.01298
                  112857.1622
                  107251.2941
                  100234.4621


                  35308.06499
                  15761.42437
                   17791.2811


                  2105.317864
                  9296.293129
                  8597.508422
FX (N)                FY (N)     FZ (N)    MX (N-M)
                0      0.41933         0            -68.8
                0      0.41933         0            -68.8
         -1.3369       0.41933   -191.55         -198.22
         -1.3369             0         0                0
         -1.3369             0         0                0
          -4.593    -1.389867          0        -196.367
          -4.593    -1.389867          0        -196.367
          -4.593    -1.389867          0        -196.367
             5.93            0         0                0
             5.93            0         0                0
             5.93   0.9705333    -75.138       -177.6587
                0   0.9705333          0       -109.7867
                0   0.9705333          0       -109.7867
                                   Applied Tip Nodal Loads with Mass (-1.5G)
MY (N-m)               MZ (N-m)      Node       FX (N)     FY (N)     FZ (N)
                   0     0.94124        9198            0 0.41933            0
                   0     0.94124        9197            0 0.41933            0
           -512.7133     0.94124        6031     -1.3369 0.41933       76.618
           -214.5033     0.94124        6099     -1.3369          0          0
           -214.5033     0.94124        6100     -1.3369          0          0
            -612.733     5.60933        6101      -4.593 -1.38987            0
            -612.733     5.60633        6102      -4.593 -1.38987            0
            -612.733     5.60633        6103      -4.593 -1.38987            0
            -389.433    -1.90056        6104         5.93         0          0
            -389.433    -1.90056        6105         5.93         0          0
            -556.413    -1.90056        6032         5.93 0.970533     30.055
                   0    -1.97053        7197            0 0.970533           0
                   0    -1.90056        7198            0 0.970533           0
MX (N-M) MY (N-m) MZ (N-m)
     -68.8        0 0.94124
     -68.8        0 0.94124
  -17.031 -95.2233 0.94124
         0 -214.503 0.94124
         0 -214.503 0.94124
 -196.367 -612.733 5.60933
 -196.367 -612.733 5.60633
 -196.367 -612.733 5.60633
         0 -389.433 -1.90056
         0 -389.433 -1.90056
 -82.6377 -322.641 -1.90056
 -109.787         0 -1.97053
 -109.787         0 -1.90056
                                                                  2
Wing Model Point Mass Loads                             36.8325 m/s
LE Mass Loads                            3.75 G Applied Loads
         Rib         Mass (kg)   Node       3.75 G Force (N)      FZ (N)    MX (N-m) MY (N-m)
                  5 13.79437        1155          -508.0811533      -295.92   296.29   -204.83
                                    1156                            -212.16   251.09   -171.08
                  6 14.51386        1153           -534.581679      -309.52   308.08   -213.11
                                    1154                            -225.06   263.22   -179.38
                  7 26.93789        1152          -992.1896947      -586.58   571.92   -388.45
                                    1151                            -405.61   473.59   -321.66
                  8 26.65452        3362          -981.7525438      -598.39     566.5  -384.76
                                    3365                            -383.36   451.77   -306.84
                  9 26.37115        3358          -971.3153929      -591.25     553.8  -376.14
                                    3361                            -380.07   442.91   -300.82
                 10 26.08778        3354          -960.8782421      -584.08   541.12   -367.53
                                    3357                             -376.8   434.02   -294.78
                 11 25.80441        3350          -950.4410912       -576.9   528.48   -358.94
                                    3353                            -373.54   425.09   -288.72
                 12 25.52105        3346          -940.0039403       -569.7   515.87   -350.38
                                    3349                            -370.31   416.14   -282.64
                 13 25.19739        3342          -928.0828344       -561.3   500.43   -339.89
                                    3345                            -366.79   405.19    -275.2
                 14 24.87373        3338          -916.1617284      -552.86   485.05   -329.44
                                    3341                             -363.3   394.21   -267.75
                 15 24.64341        3334          -907.6784518      -546.84   474.15   -322.04
                                    3337                            -360.84   386.38   -262.43
                 16 24.41376        3330          -899.2199077      -540.81   463.32   -314.68
                                    3333                            -358.41   378.57   -257.12
                 17 24.18344        3326           -890.736631      -534.74     452.5  -307.34
                                    3329                               -356   370.74   -251.81
                 18 23.95312        3322          -882.2533544      -528.65   441.74   -300.03
                                    3325                             -353.6   362.92   -246.49
                 19 23.72347        3318          -873.7948103      -522.56   431.07   -292.78
                                    3321                            -351.24   355.13    -241.2
                 20 23.49315        3314          -865.3115337      -516.42   420.43   -285.55
                                    3317                            -348.89   347.34   -235.91
                 21   23.2635       3310          -856.8529896      -510.27   409.88   -278.39
                                    3313                            -346.58     339.6  -230.66
                 22 23.03318        3306           -848.369713      -504.37   399.61   -271.41
                                    3309                            -344.48   332.06   -225.53
                 23 22.80286        3302          -839.8864363      -497.86   388.96   -264.18
                                    3305                            -342.03   324.18   -220.18
                 24 22.57321        3298          -831.4278922      -491.62   378.65   -257.18
                                    3301                            -339.81   316.56   -215.01
                 25 22.34289        3294          -822.9446156      -485.33     368.4  -250.21
                                    3297                            -337.62   308.97   -209.85
                 26 22.11324        6085          -814.4860715      -479.01   358.26   -243.33
                                       6088                           -335.48   301.46    -204.75
                  27 21.88292          6081          -806.0027949     -472.63    348.2    -236.49
                                       6084                           -333.37     294     -199.68
                  28   21.6526         6077          -797.5195182     -466.19   338.23    -229.73
                                       6080                           -331.32   286.61    -194.67
                  29 21.42295          6073          -789.0609742     -459.72    328.4    -223.05
                                       6076                           -329.34   279.33    -189.72
                  30 21.19263          6069          -780.5776975     -453.16   318.64    -216.42
                                       6072                           -327.41   272.12    -184.82
                  31 20.96299          6065          -772.1191534     -446.55   308.81    -210.21
                                       6068                           -325.57   264.84    -180.28
                  32 20.73266          6061          -763.6358768     -439.84    299.5    -203.42
                                       6064                            -323.8   258.02    -175.24
                  33 20.62254          6057          -759.5797329     -436.59   294.98    -200.35
                                       6060                           -322.99   254.71       -173
                  34 20.51175          6053          -755.4988563      -433.3   290.47    -197.28
                                       6056                           -322.19   251.41    -170.75
                  35 20.26598          6049          -746.4467302     -425.92   280.55    -190.55
                                       6052                           -320.53   244.18    -165.85
                  36 20.01954          6045          -737.3698715     -418.37   270.74    -183.89
                                       6048                              -319    237.1    -161.03
                  37 19.77378          6041          -728.3177454     -410.69    261.1    -177.34
                                       6044                           -317.63   230.19    -156.34
                  38 19.52802          6037          -719.2656193     -402.81    251.6    -170.88
                                       6040                           -316.45   223.46    -151.77
                  39 19.28158          6033          -710.1887606     -394.71   242.22    -164.51
                                       6036                           -315.48    216.9    -147.32
                  40 16.42816          6031          -605.0903109     -333.47   201.09    -136.58
                                       6030                  6030     -271.62   181.71    -123.41

TE Flaps/Spoilers/Ailerons Mass Loads        3.75 G Applied Loads
          Rib           Mass (kg)    Node       3.75 G Force (N)     FZ (N)   MX (N-m) MY (N-m)
                     9                  3359                          -966.26  -1513.6   1001.8
                                        3360                          -743.25  -1357.7   897.72
                        35.43895                      -1305.305202
                        10.97411                       -404.203773
                    10                  3355                          -959.59   -1456.5   964.69
                                        3356                          -731.55   -1303.8   862.64
                        35.05815                      -1291.279204
                        10.85619                      -399.8604508
                    11                  3351                          -953.02   -1400.1   927.58
                                        3352                          -719.75   -1250.5   827.61
                        34.67734                      -1277.253207
                        10.73826                      -395.5171285
                    12                  3347                          -946.51   -1344.3   891.26
                                        3348                          -707.89   -1197.9   793.41
                        34.29654                      -1263.227209
     10.62034          -391.1738063
13              3343                  -939.81   -1274.9    845.7
                3344                  -693.61   -1132.5   750.44
     33.86159          -1247.206994
     10.48566          -386.2129501
14              3339                  -1096.7   -1443.9   957.54
                3340                  -802.68   -1283.1   849.92
     38.64652          -1423.447993
     12.92196          -475.9479156
15              3335                  -436.58   -467.84   311.82
                3336                  -300.62   -399.49     266
     17.46766          -643.3776235
     2.547179          -93.81897785
16              3331                  -434.63   -448.18   298.88
                3332                   -295.7   -381.43    254.1
     17.30488          -637.3820664
     2.523442          -92.94469031
17              3327                  -1080.4   -1272.5   845.43
                3328                  -766.28   -1122.8   744.95
     37.57401          -1383.944811
     12.56335          -462.7395249
18              3323                  -915.01   -1015.9   675.51
                3324                  -637.75   -890.66   591.39
     32.18948          -1185.618905
     9.967866          -367.1414426
19              3319                  -910.51   -969.55   644.94
                3320                  -627.36   -847.85   563.15
     31.88086          -1174.251865
       9.8723           -363.621499
20              3315                  -905.97   -923.51   614.47
                3316                  -616.97   -805.57   535.15
     31.57135          -1162.851587
     9.776455          -360.0912632
21              3311                  -901.38   -877.99   584.53
                3312                  -606.67      -764   507.79
     31.26273          -1151.484546
     9.680888          -356.5713195
22              3307                  -896.69   -832.77   554.81
                3308                  -596.43   -722.97    480.8
     30.95321          -1140.084269
     9.585043          -353.0410837
23              3303                  -891.87   -787.94   525.51
                3304                  -586.33   -682.59   454.36
      30.6437          -1128.683991
     9.489197          -349.5108478
24              3299                  -886.89   -743.78    496.5
                3300                  -576.41   -643.08   428.41
     30.33508          -1117.316951
     9.393631          -345.9909042
25              3295                  -881.68   -699.96   467.66
                3296                   -566.7   -604.18   402.78
     30.02557          -1105.916673
     9.297785          -342.4606683
26              6086                  -876.22   -656.72    439.3
                6087                  -557.27   -566.12    377.8
     29.71695          -1094.549632
     9.202219          -338.9407247
27              6082                  -870.43   -613.87    411.2
                6083                  -548.13    -528.7   353.25
     29.40744          -1083.149355
     9.106373          -335.4104888
28              6078                  -864.28    -571.6   383.35
                6079                  -539.35   -492.09    329.1
     29.09792          -1071.749077
     9.010527           -331.880253
29              6074                  -857.76   -529.96   356.18
                6075                  -530.98    -456.3   305.78
      28.7893          -1060.382036
     8.914961          -328.3603094
30              6070                  -850.82   -488.79   329.36
                6071                     -523   -421.19   282.88
     28.47979          -1048.981759
     8.819116          -324.8300735
31              6066                  -843.48   -448.44   303.05
                6067                  -515.44      -387    260.6
     28.17117          -1037.614718
     8.723549          -321.3101299
32              6062                  -983.41   -492.76   333.84
                6063                  -603.06    -428.1   288.91
      32.2724          -1188.673186
     10.80016          -397.7968882
33              6058                  -332.29   -133.21   91.485
                6059                  -191.98   -111.88   76.528
     12.07416          -444.7214972
     2.159963          -79.55684285
34              6054                  -330.63   -126.46   87.106
                6055                  -190.73   -106.45    73.01
     12.00749          -442.2657619
      2.14747          -79.09669151
35              6050                  -326.84   -111.79   77.749
                6051                  -188.07   -94.678   65.531
     11.85977          -436.8251001
     2.119846          -78.07924578
36              6046                  -322.92   -97.614   68.845
                                       6047                         -185.51   -83.366       58.472
                       11.71167                   -431.370027
                       2.092153                  -77.05924366
                  37                   6042                         -318.95   -84.147       60.742
                                       6043                         -183.02   -72.694       52.144
                       11.56395                  -425.9293653
                        2.06453                  -76.04179792
                  38                   6038                         -315.43   -77.542       44.632
                                       6039                         -180.81    -68.12       39.459
                       11.42963                  -420.9817782
                         2.0435                  -75.26720984
                  39                   6034                          -264.1   -186.91       122.78
                       11.26814        6035      -489.0379805       -224.94   -172.45       113.28
                       2.009213
                  40                   6032                         -224.62   -137.73       90.518
                       9.779729        6029       -408.876713       -184.26   -124.79       82.014
                       1.321248

Total Tip Mass Loads 3.75 G Applied Loads                       -1.5 G Applied Loads
         Nodes         FZ (N)    MX (N-m)      MY (N-m)             FZ (N)    MX (N-m) MY (N-m)
                 6030    -459.4       53.53           -418.31        183.762    -21.412 167.326
                 6031   -525.02       71.67           -434.79        210.008    -28.665  173.91
                 6029 -258.919     -192.373           -84.276        103.567     76.949    33.71
                 6032 -299.758     -205.602           -76.462        119.903     82.241  30.585

Total LG Mass Loads 3.75 G Applied Loads                                                -1.5 G Applied Loads
        Nodes         FY (N)      FZ (N)       MX (N-m)       MY (N-m) MZ (N-m)            FY (N)
                  431   49.121      -20038             -32464   -8223.8   17706             -19.649
                  430  -256.16      -17314             -29651   -6628.2  -17247              102.46
                 3347   54.109 -281046.51            -20571.3 276911.26  1472.8             -21.645
                 3348   152.93 -195887.89            -16665.9 223343.41 -952.36             -61.169

                      3
Total Engine Mass Loads.75 G Applied Loads
        Nodes           FX (N)      FY (N)      FZ (N)           MX (N-M) MY (N-M) MZ (N-M)
                3339      787.29      9610.6          33603.3     -25875.9 3418.04   -127.56
                3982     -3006.2      -30815          -1115.1        64713  -6520.3   -662.3
                3346      2218.9       21205        -231099.7    245185.87 -25011.4  -8.1335
                        2
          -14.733 m/s
-1.5 G Applied Loads
 -1.5 G Force (N)           FZ (N)            MX (N-m) MY (N-m)
     203.2324613                     118.37    -118.52   81.934
                                     84.866    -100.43   68.434
    213.8326716                      123.81    -123.23   85.242
                                     90.026    -105.29   71.753
    396.8758779                      234.63    -228.77   155.38
                                     162.24    -189.43   128.66
    392.7010175                      239.36      -226.6    153.9
                                     153.34    -180.71   122.74
    388.5261572                       236.5    -221.52   150.45
                                     152.03    -177.17   120.33
    384.3512968                      233.63    -216.45   147.01
                                     150.72    -173.61   117.91
    380.1764365                      230.76    -211.39   143.58
                                     149.42    -170.04   115.49
    376.0015761                      227.88    -206.35   140.15
                                     148.12    -166.46   113.06
    371.2331337                      224.52    -200.17   135.96
                                     146.71    -162.08   110.08
    366.4646914                      221.14    -194.02   131.78
                                     145.32    -157.68     107.1
    363.0713807                      218.73    -189.66   128.81
                                     144.34    -154.55   104.97
    359.6879631                      216.32    -185.33   125.87
                                     143.37    -151.43   102.85
    356.2946524                       213.9        -181  122.93
                                      142.4      -148.3  100.72
    352.9013418                      211.46      -176.7  120.01
                                     141.44    -145.17   98.597
    349.5179241                      209.02    -172.43   117.11
                                      140.5    -142.05   96.481
    346.1246135                      206.57    -168.17   114.22
                                     139.56    -138.94   94.365
    342.7411958                      204.11    -163.95   111.36
                                     138.63    -135.84   92.262
    339.3478852                      201.63    -159.75     108.5
                                     137.71    -132.75   90.162
    335.9545745                      199.14    -155.58   105.67
                                     136.81    -129.67   88.073
    332.5711569                      196.65    -151.46   102.87
                                     135.92    -126.62   86.002
    329.1778462                      194.13    -147.36   100.09
                                     135.05    -123.59     83.94
    325.7944286                       191.6    -143.31   97.332
                                134.19   -120.58     81.9
     322.401118                 189.05   -139.28   94.598
                                133.35    -117.6   79.873
    319.0078073                 186.48   -135.29    91.89
                                132.53   -114.65   77.867
    315.6243897                 183.89   -131.36   89.219
                                131.74   -111.73   75.888
     312.231079                 181.27   -127.46   86.569
                                130.97   -108.85   73.929
    308.8476614                 178.62   -123.52   84.086
                                130.23   -105.93   72.113
    305.4543507                 175.93    -119.8   81.367
                                129.52   -103.21   70.098
    303.8318931                 174.64   -117.99    80.14
                                 129.2   -101.88   69.199
    302.1995425                 173.32   -116.19   78.913
                                128.88   -100.56   68.301
    298.5786921                 170.37   -112.22   76.219
                                128.21   -97.674    66.34
    294.9479486                 167.35    -108.3   73.554
                                 127.6   -94.838   64.414
    291.3270982                 164.27   -104.44   70.935
                                127.05   -92.076   62.538
    287.7062477                 161.13   -100.64   68.354
                                126.58   -89.384   60.709
    284.0755043                 157.89   -96.886   65.805
                                126.19   -86.759   58.926
    242.0361244                 133.39   -80.434    54.63
                                108.65   -72.683   49.366

-1.5 G Applied Loads
 -1.5 G Force (N)      FZ (N)          MX (N-m) MY (N-m)
                                 386.5   605.45    -400.7
                                 297.3   543.09  -359.09
    522.1220808
    161.6815092
                                383.84    582.6    -385.87
                                292.62    521.5    -345.06
    516.5116818
    159.9441803
                                381.21   560.04    -371.03
                                 287.9   500.21    -331.05
    510.9012828
    158.2068514
                                 378.6   537.72     -356.5
                                283.16   479.17    -317.36
    505.2908837
156.4695225
              375.92   509.96   -338.28
              277.45   453.01   -300.17
498.8827977
  154.48518
              438.69   577.57   -383.02
              321.07   513.25   -339.97
569.3791971
190.3791662
              174.63   187.14   -124.73
              120.25    159.8    -106.4
257.3510494
37.52759114
              173.85   179.27   -119.55
              118.28   152.57   -101.64
254.9528265
37.17787613
              432.16   508.99   -338.17
              306.51    449.1   -297.98
553.5779242
  185.09581
              366.01   406.38   -270.21
               255.1   356.27   -236.56
474.2475622
146.8565771
               364.2   387.82   -257.98
              250.95   339.14   -225.26
469.7007459
145.4485996
              362.39    369.4   -245.79
              246.79   322.23   -214.06
465.1406348
144.0365053
              360.55   351.19   -233.81
              242.67    305.6   -203.12
460.5938186
142.6285278
              358.68   333.11   -221.92
              238.57   289.19   -192.32
456.0337075
141.2164335
              356.75   315.18   -210.21
              234.53   273.04   -181.74
451.4735965
139.8043391
              354.76   297.51    -198.6
              230.57   257.23   -171.36
446.9267802
138.3963617
              352.67   279.98   -187.06
              226.68   241.67   -161.11
442.3666692
136.9842673
              350.49   262.69   -175.72
              222.91   226.45   -151.12
437.8198529
135.5762899
              348.17   245.55   -164.48
              219.25   211.48    -141.3
433.2597418
134.1641955
              345.71   228.64   -153.34
              215.74   196.83   -131.64
428.6996308
132.7521012
               343.1   211.98   -142.47
              212.39   182.52   -122.31
424.1528145
131.3441237
              340.33   195.52   -131.74
               209.2   168.48   -113.15
419.5927035
129.9320294
              337.39   179.38   -121.22
              206.18    154.8   -104.24
415.0458872
 128.524052
              393.37    197.1   -133.54
              241.22   171.24   -115.56
475.4692745
159.1187553
              132.92   53.283   -36.594
              76.793    44.75   -30.611
177.8885989
31.82273714
              132.25   50.586   -34.842
              76.292   42.578   -29.204
176.9063047
31.63867661
              130.74   44.717     -31.1
              75.227   37.871   -26.213
174.7300401
31.23169831
              129.17   39.046   -27.538
                                             74.203     33.346   -23.389
                172.5480108
                30.82369746
                                             127.58     33.659   -24.297
                                             73.206     29.077   -20.857
                170.3717461
                30.41671917
                                             126.18     31.017   -17.853
                                             72.322     27.248   -15.784
                168.3927113
                30.10688394
                                             105.64     74.763   -49.113
                195.6151922                  89.977     68.979   -45.314

                                             89.848     55.092   -36.207
                163.5506852                  73.703     49.916   -32.806




-1.5 G Applied Loads
                  FZ (N)          MX (N-m)            MY (N-m) MZ (N-m)
                       8015.3                12986        3289.5   -7082
                       6925.6                11861        2651.3  6898.8
                    112418.6                8228.62     -110767  -589.14
                    78354.16                6666.47    -89338.4   380.94

           -1.5 G Applied Loads
                 FX (N)            FY (N)            FZ (N) MX (N-m) MY (N-m) MZ (N-m)
                     -314.92                -3844.2 -13441.3 10350.27 -1367.21  51.026
                      1202.5                 12326    446.04   -25885   2608.1  264.92
                     -887.57                -8481.8 92439.88 -98073.4 10004.45  3.2534
Volume ID Volume (m^3) Fuel Load (N) Fuel Mass (kg) Cell Lower Area (m^2)
         1        4.479 35317.37007       3595.7412                   3.881
         2        4.674 36854.96488       3752.2872                   3.881
         3        4.441 35017.73621       3565.2348                   3.881
         4       0.7162 5647.309766       574.96536                  0.6002
         5          2.18 17189.52149       1750.104                   1.799
         6        3.446 27172.06011       2766.4488           2.997917662
         7        2.987 23552.79848       2397.9636               2.829076
         8        2.645 20856.09373        2123.406                   2.612
         9        2.517 19846.80073       2020.6476                     2.55
       10         2.392 13202.81412       1920.2976                   2.488
       11           2.27 12529.42644       1822.356                   2.426
       12         2.777    15327.849      2229.3756                   3.065
       13         2.582 20359.33233       2072.8296                     2.96
       14         1.723 13586.03006       1383.2244                   2.043
       15         1.626   12821.1752      1305.3528                   1.984
       16         1.541 12150.94157       1237.1148                   1.937
       17         1.454 11464.93773       1167.2712                   1.883
       18         1.366 10771.04879       1096.6248                   1.825
       19         1.288 10156.01086       1034.0064                   1.777
       20         1.205 9501.547428         967.374                   1.719
       21         1.131   8918.04991       907.9668                   1.671
       22         1.057 8334.552391        848.5596                   1.618
       23        0.9818 7741.592751       788.18904                     1.56
       24        0.9152 7216.444984       734.72256                   1.512
       25        0.8459 6670.007443       679.08852                   1.454
       26         0.784 6181.919654        629.3952                   1.406
       27        0.7222 5694.620376       579.78216                   1.352
       28        0.6609 5211.263647       530.57052                   1.296
       29        0.6061   4779.16008      486.57708                   1.246
       30        0.5503   4339.17141      441.78084                     1.19
       31        0.5002   3944.12782      401.56056                     1.14
       32        0.2216 1747.338515       177.90048                  0.5263
       33        0.2119 1670.853029       170.11332                  0.5173
       34        0.4318 3404.786871       346.64904                   1.104
       35        0.3825 3016.051362         307.071                   1.046
       36        0.3342 2635.200955       268.29576                  0.9823
       37        0.2902 2288.256484       232.97256                  0.9218
       38        0.2498   1969.69838      200.53944                  0.8636
       39        0.2112 1665.333458       169.55136                  0.8006
Fuel Load 3.75 G (N) Fuel Load -1.5 G (N)   Total Pressure 3.75 G (N/m^2)
        132440.1377          -52976.0551                       34125.26095
        138206.1183         -55282.44732                        35610.9555
        131316.5108         -52526.60431                       33835.74099
        21177.41162         -8470.964649                       35283.92473
        64460.70558         -25784.28223                       35831.40944
        101895.2254         -40758.09017                       33988.66711
         88322.9943         -35329.19772                       31219.73192
         78210.3515          -31284.1406                       29942.70731
        74425.50273         -29770.20109                       29186.47166
        70729.36135         -28291.74454                        28428.1999
        67121.92737         -26848.77095                       27667.73593
        82113.47679         -32845.39071                       26790.69389
        76347.49624          -30538.9985                       25793.07305
        50947.61271         -20379.04509                       24937.64695
        48079.40701          -19231.7628                       24233.57208
        45566.03087         -18226.41235                       23524.02213
        42993.51647         -17197.40659                       22832.45697
        40391.43295         -16156.57318                       22132.29203
        38085.04073         -15234.01629                         21432.212
        35630.80286         -14252.32114                       20727.63401
        33442.68716         -13377.07486                         20013.577
        31254.57147         -12501.82859                       19316.79324
        29030.97282         -11612.38913                       18609.59796
        27061.66869         -10824.66748                       17897.92903
        25012.52791         -10005.01117                        17202.5639
         23182.1987         -9272.879482                       16488.05029
        21354.82641         -8541.930563                       15794.98995
        19542.23868         -7816.895471                       15078.88787
         17921.8503          -7168.74012                       14383.50746
        16271.89279         -6508.757116                       13673.85949
        14790.47933          -5916.19173                       12974.10467
         6552.51943         -2621.007772                       12450.16042
        6265.698859         -2506.279544                       12112.31173
        12767.95077         -5107.180306                        11565.1728
        11310.19261         -4524.077043                       10812.80364
         9882.00358         -3952.801432                       10060.06676
        8580.961816         -3432.384726                       9308.919306
        7386.368924          -2954.54757                       8552.997827
        6245.000467         -2498.000187                       7800.400284
  Total Pressure -1.5 G (N/m^2) Height (m)         KP*   Z Coord. (m)
                    -13650.10438         0.9146       16    0.3780203
                      -14244.3822        0.9146        3    0.3780203
                    -13534.29639         0.9146        7    0.3780203
                    -14113.56989            1.12     147    0.4715195
                    -14332.56378          1.147      155    0.4878046
                    -13595.46684          1.145      152    0.5056829
                    -12487.89277         0.9146      148    0.3780203
                    -11977.08292         0.8015      143    0.2787386
                    -11674.58866         0.7814      139    0.2717297
                    -11371.27996         0.7612      135    0.2647207
                    -11067.09437         0.7411      131    0.2577118
                    -10716.27756         0.7209      127    0.2507028
                    -10317.22922         0.6947      123    0.2415804
                    -9975.058779         0.6684      119     0.232458
                    -9693.428832         0.6498      115    0.2259664
                    -9409.608853         0.6312      111    0.2194936
                    -9132.982788         0.6125      107     0.213002
                      -8852.91681        0.5938      103    0.2065103
                    -8572.884801         0.5752       99    0.2000376
                    -8291.053602         0.5566       95    0.1935459
                    -8005.430799         0.5379       91    0.1870732
                    -7726.717297         0.5193       87    0.1805815
                    -7443.839184         0.5006       83    0.1740899
                    -7159.171611          0.482       79    0.1676171
                    -6881.025561         0.4633       75    0.1611255
                    -6595.220115         0.4447       71    0.1546527
                    -6317.995979          0.426       67    0.1481611
                    -6031.555148         0.4074       63    0.1416694
                    -5753.402985         0.3888       59    0.1351967
                    -5469.543795         0.3701       55     0.128705
                    -5189.641869         0.3515       51 0.12222323
                    -4980.064168         0.3328       47    0.1157406
                    -4844.924693         0.3239       43    0.1126368
                    -4626.069118         0.3149       39    0.1095139
                    -4325.121456          0.295       35     0.102587
                    -4024.026705          0.275       31    0.0956411
                    -3723.567722         0.2551       27 0.08871414
                    -3421.199131         0.2352       23 0.08178717
                    -3120.160114         0.2152       19 0.07484129
*Inboard TE line or smallest inboard line height
  Common Rib Net Pressure 3.75G (N/m^2)     Common Rib Net Pressure -1.5G (N/m^2)
                              2724.065274                               -1089.62611
                              905.8774897                              -362.3509959
                             -1082.407462                               432.9629848
                              1081.310527                              -432.5242108
                              418.6433081                              -167.4573232
                             -1406.626647                               562.6506588
                             -1688.312082                               675.3248328
                             -682.3568155                               272.9427262
                             -393.9483594                               157.5793438
                             -384.7976411                               153.9190564
                             -375.7198982                               150.2879593
                              -421.506403                               168.6025612
                              -462.031465                                184.812586
                             -381.1778735                               152.4711494
                             -305.0052326                                122.002093
                             -298.5786177                               119.4314471
                             -282.3891082                               112.9556433
                             -277.1719627                               110.8687851
                             -268.4573528                               107.3829411
                             -261.4454088                               104.5781635
                             -256.0608434                               102.4243373
                             -241.2265355                               96.49061419
                             -236.0146395                               94.40585578
                             -228.6829496                               91.47317984
                             -214.7751089                               85.91004356
                             -211.8294695                                84.7317878
                             -196.8291367                               78.73165467
                             -194.4933244                               77.79732977
                             -180.2426011                               72.09704045
                             -175.0938107                               70.03752428
                             -163.9758782                                65.5903513
                             -116.2457645                                46.4983058
                             -72.95279362                               29.18111745
                             -114.8627008                               45.94508032
                             -147.9659338                               59.18637353
                              -138.001761                                55.2007044
                              -127.745144                                51.0980576
                             -118.5284878                               47.41139513
                             -107.9726609                               43.18906437
Rib 4 common pressure
Wing Model Emergency Landing Loads
Wing box mass and engine mass only
 Position   Link     Mass (kg) -6G Force (N)   9G Force (N) 3G Force (N)
TE                1 101.7525      5996.47833   -8994.717495 -2998.239165 Node
Joint TE          2 203.505 11992.95666        -17989.43499 -5996.47833 3339
Mid               3
Joint LE          4 305.2575 17989.43499       -26984.15249 -8994.717495 3982
LE                5
Engine CG              4736.51 279132.0073      -418698.011 -139566.0037 3346
 Emergency Reaction Loads                                                    Gravity Axis
FX (N)                     FY (N)    FZ (N)    MX (N-M) MY (N-M) MZ (N-M)    6G      z
                 -16208.98 -16017.1 -25036.3     11378.3   -903.68 -5817.396 9G      y
                                                                             3G      x
                   -372964      12766 30712.66    -92482 -289926.6 -74002.02

                 51150.72 -448637.2   309780    -16118    83936.2 21949.0136
Value (N/m^2)
        58.932
        88.398
        29.466

				
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