Deformed geometries
The CAD models correspond to the NASA-CRM wing-body-horizontal tail.
The wing geometry accounts for the experimentally measured deformation.
Reference Area, S = 594,720.0 in2
Reference Chord, c = 275.80 in
Reference Span, b = 2,313.50 in
Moment Reference (X,Y,Z) = (1,325.90, 468.75, 177.95) in
IGES Files
| Angle of attack | File |
| 4.84deg | wbh_aoa484_buffet_deformed.iges.gz |
| 5.89deg | wbh_aoa589_buffet_deformed.iges.gz |
Deformation informations
Deformation is considered only in the z-direction.
The deformation is averaged over 10 images (more info will be added).
| Position before deformation | AoA = 4.84deg | AoA = 5.89deg | |||||
| Marker ID | x[mm] | y[mm] | z[mm] | Δz[mm] | Δα[deg] | Δz[mm] | Δα[deg] |
| 201 | 558.610 | 105.191 | -15.721 | 0.295 | 0.287 | ||
| 202 | 651.608 | 105.191 | -22.207 | 0.382 | -0.021 | 0.393 | -0.028 |
| 203 | 744.183 | 105.191 | -35.747 | 0.360 | 0.374 | ||
| 204 | 632.574 | 215.746 | -16.204 | 0.447 | 0.450 | ||
| 205 | 699.777 | 215.746 | -16.136 | 0.600 | -0.127 | 0.600 | -0.132 |
| 206 | 766.844 | 215.746 | -23.570 | 0.746 | 0.759 | ||
| 207 | 729.204 | 350.702 | -9.925 | 1.373 | 1.414 | ||
| 208 | 780.545 | 350.702 | -7.286 | 1.718 | -0.418 | 1.779 | -0.423 |
| 209 | 832.002 | 350.702 | -11.605 | 2.122 | 2.173 | ||
| 210 | 836.606 | 498.954 | 5.173 | 4.345 | 4.438 | ||
| 211 | 873.418 | 498.954 | 7.676 | 4.819 | -0.722 | 4.913 | -0.721 |
| 212 | 910.394 | 498.954 | 5.397 | 5.273 | 5.365 | ||
| 213 | 880.023 | 558.864 | 13.814 | 5.977 | 6.094 | ||
| 214 | 910.963 | 558.864 | 16.284 | 6.364 | -0.773 | 6.456 | -0.784 |
| 215 | 942.081 | 558.864 | 14.538 | 6.812 | 6.940 | ||
| 216 | 923.446 | 618.774 | 23.298 | 7.689 | 7.799 | ||
| 217 | 948.521 | 618.774 | 25.615 | 7.984 | -0.774 | 8.111 | -0.769 |
| 218 | 973.781 | 618.774 | 24.835 | 8.364 | 8.470 | ||
| Δz | : Amount of deflection |
| Δα | : Amount of torsion |
*The above values are measured on the 2.16% model using JAXA wind tunnel test.
