摘要
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 effects of spinning on the aerodynamic characteristics.ofthe wing-body combinations are studied.The model for calculating the aerodynamiccharacteristics of spinning wing-body combinations is established and the method offinite elementary solution as forwarded by F.A.Woodward is used to calculate theaerodynamic characteristics of spinning wing-body combinations at supersonic speed.
出处
《弹道学报》
EI
CSCD
1993年第2期21-32,共12页
Journal of Ballistics
关键词
空气动力特性
旋转翼-身
组合体
aerodynamic characteristics
the method of finite elementary solution
panel method
calculation aerodynamics
spinning effects
numerical calculation
