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该文分析了旋转对翼-身组合体空气动力特性的影响,建立了旋转翼-身组合体空气动力特性的数值计算模型,采用伍德沃德(Woodward)有限基本解方法(面元法),计算了旋转翼-身组合体超音速空气动力特性.
In this paper, the aerodynamic characteristics of a rotating wing-body combination are analyzed. A numerical calculation model of the aerodynamic characteristics of a rotating wing-body combination is established. Woodward finite element method (face-element method) The supersonic aerodynamic characteristics of the rotating wing-body combination are calculated.