翼轮廓
EXPERIMENTAL INVESTIGATION OF THE INTERFERENCE AERODYNAMICS OF CLOSE-COUPLED CANARD CONFIGURATION On the basis of the canard configuration a contour stealthy design including chiefly the wing, the fuselage and their connection type is projected.
近耦鸭式布局干扰气动力实验研究在鸭式布局的基础上,对飞行器各部件及部件间的连接方式进行了外形隐身设计。
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