This thesis is aimed the wing-rotor aerodynamic interaction of the compound helicopter in hover.
本文就复合式直升机在悬停状态下的旋翼/机翼之间的气动干扰问题进行了较为深入的研究。
参考来源 - 复合式高速直升机悬停状态旋翼/机翼气动干扰研究·2,447,543篇论文数据，部分数据来源于NoteExpress
A full coupled and iterative analytical method has been developed to investigate the aerodynamic interaction of a helicopter fuselage on its rotor.
建立了一个全耦合的机身对旋翼气动干扰的迭代计算方法。
Research on the aerodynamic interaction between the rotors and components of rotorcraft have been a very important aspect and a very challenging subject in rotorcraft Aerodynamics.
旋翼干扰空气动力学问题一直是旋翼飞行器空气动力学的研究热点和难点之一。
The aerodynamic pressure expression at jet location and in the area of jet interaction is established by blast wave principium.
采用爆炸波原理建立了喷流区和喷流干扰区的气动压力计算模型。
应用推荐