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
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。
A full coupled and iterative analytical method has been developed to investigate the aerodynamic interaction of a helicopter fuselage on its rotor.
试验结果表明：对于本模型喷流气动干扰使喷流放大因子略有变化；
The results of the experiment is:(1) the amplification factor changes little because of the interferences of the lateral jet;
对各列叶栅的非定常气动力和气动力矩进行频谱分析，探讨叶列间的非定常气动干扰。
Through spectrum analysis of the unsteady aerodynamic forces and moments of each blade cascade, the unsteady aerodynamic interferences between blades were discussed.
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