Research Article
Static Aeroelastic Modeling and Rapid Analysis of Wings in Transonic Flow
Table 8
The comparison of the aerodynamic force coefficient by the CFD/CSD method and modeling method.
| | Dynamic pressure (Pa) | CL (CFD) | CL (model) | CL (error) | CD (CFD) | CD (model) | CD (error) |
| | 20,000 | 0.387007 | 0.38864 | +0.42% | 0.023206 | 0.023548 | +1.47% | | 40,055.4 | 0.378365 | 0.38004 | +0.44% | 0.022848 | 0.023065 | +0.95% | | 50,000 | 0.374299 | 0.37583 | +0.41% | 0.022695 | 0.022903 | +0.92% | | 60,000 | 0.370305 | 0.37172 | +0.38% | 0.022549 | 0.022765 | +0.96% | | 80,000 | 0.362644 | 0.36397 | +0.37% | 0.022267 | 0.022462 | +0.88% |
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