Research Article
Experimental and Numerical Studies on Static Aeroelastic Behaviours of a Forward-Swept Wing Model
Table 4
Wing tip displacements when
, semispan.
| q (Pa) | LE | TE | VLM + linear | VLM + nonlinear | Experiment | CFD/CSD | VLM + linear | VLM + nonlinear | Experiment | CFD/CSD |
| 117 | 2.13 | 2.13 | 2.57 | 2.51 | 1.78 | 1.78 | 1.90 | 2.11 | 153 | 3.22 | 3.22 | 3.42 | 3.88 | 2.70 | 2.70 | 2.92 | 3.25 | 194 | 4.97 | 4.96 | 5.44 | 6.16 | 4.16 | 4.16 | 4.50 | 5.17 | 216 | 6.27 | 6.23 | 6.77 | 7.90 | 5.25 | 5.22 | 5.69 | 6.62 | 239 | 8.06 | 7.92 | 9.62 | 10.33 | 6.75 | 6.64 | 8.25 | 8.66 | 251 | 9.24 | 9.01 | 11.57 | 12.01 | 7.73 | 7.54 | 9.76 | 10.07 | 264 | 10.78 | 10.37 | 15.05 | 15.72 | 9.03 | 8.69 | 12.71 | 13.19 | 276 | 12.55 | 11.85 | 18.69 | 16.75 | 10.51 | 9.92 | 15.81 | 14.07 | 289 | 14.98 | 13.71 | 21.75 | 21.25 | 12.54 | 11.49 | 18.62 | 17.89 | 310 | 20.74 | 17.42 | | 28.81 | 17.37 | 14.60 | | 24.30 | 324 | 26.91 | 20.42 | | 32.50 | 22.52 | 17.12 | | 27.42 | 338 | 36.98 | 23.84 | | 35.47 | 30.96 | 19.99 | | 29.93 | 352 | 56.44 | 27.62 | | 38.29 | 47.24 | 23.17 | | 32.34 | 367 | 117.30 | 31.89 | | 41.51 | 98.18 | 26.77 | | 35.07 |
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