... wings with complex taper 复杂渐尖度的机翼 wings with flaps 带襟翼的机翼 resistive drag force 阻力 ...
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数值算例表明本方法是求解带襟翼偏转的机翼绕流的有效方法。
Numerical results show that the present method is effective one for solving the flow around wing with flap deflection.
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