Hypersonic air-breathing propulsion is one of the key techniques for future aviation and the ground aerodynamic testing ......

In this paper a novel design method of aerodynamic configuration is proposed to inte-grate forebody,strut and inlet for ......

综述了ONERA（法国宇航院）在高超声速流中采用激光或电子束等光学技术实现非接触式精确测量上已取得的进展。点、视线和成像测量均属......

以静稳定性衡量稳定性能，以可用过载衡量机动性，给出了高超声速飞行器操稳性能的计算方法。并以高超声速飞行器基准外形为例，计算了其......

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采用自主开发的数值软件SPACER对典型气动布局在Ma=6.0(Re=1×107)高超声速巡航时的气动力性能进行了数值评估。评估的气动布局包......

A physical mechanism by which nose bluntness suppresses second-mode instability is proposed.Considered are 7 degree half......