Open Access

Table 2

The optimized parameters of the wing.

  Parameters Original Values Candidate Values
Delta wing Chord length Lc1 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 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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