Open Access
Table 2
The optimized parameters of the wing.
| Parameters | Original Values | Candidate Values | ||
|---|---|---|---|---|
| Delta wing | Chord length Lc1 | 5° | 6.9969° | |
| Sweep angle βsw1 | 1.4 m | 1.3036 m | ||
| Span of winglet spw1 | 0.85 m | 0.8520 m | ||
| Ratio of plainwing tip λ1 | 0.4 | 0.4251 | ||
| Ratio of winglet tip λsw | 0.3 | 0.3819 | ||
| Canard wing | Incident angle αin2 | 6° | 7.5149° | |
| Chord length Lc2 | 0.15 m | 0.1000 m | ||
| Span of wing sp2 | 0.6 m | 0.6450 m | ||
| Height of upper part hup | 0.5 m | 0.5519 m | ||
| Aerodynamics | Fy (N) | RSM | – | 150.1228N |
| CFD | 142.4002N | 150.0432N | ||
| Error | – | 0.05% | ||
| Fx (N) | RSM | – | 20.1402N | |
| CFD | 18.4685N | 20.1486N | ||
| Error | – | 0.04% | ||
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