windtu相关论文
An integration method based on a novel combined flow for aerodynamic configuration of strutjet engin
In this paper a novel design method of aerodynamic configuration is proposed to inte-grate forebody,strut and inlet for ......
目的 研究对气动轴不对称飞行器气动吹风安排及气动插值的方法． 方法 按照不同的气动滚转角，进行合理有限的吹风，然后以三角周期函......
