The results indicate that it is more favorable for the aerodynamic characteristics to equip a higher close canard wing together with forward-swept Angle of main wing increasing.
实验结果表明:随着主机翼前掠角的增大,近距鸭翼布置高度逐渐增加可获得较好的气动特性。
The more swept-back the wing Angle, the less the drag and the better for flight approaching supersonic speed.
越是掠翼角,少的阻力和为接近超音速飞行更好。
The method does not require to calculate the details of the stream lines and can be used for various swept wings at moderate angle of attack or yaw angle.
这种方法不需要计算出无粘流线的细节,并适用于不同外形的后掠翼。
应用推荐