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作品数：77被引量：67H指数：5
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Tomography-like flow visualization of a hypersonic inward-turning inlet被引量：8
《Chinese Journal of Aeronautics》2021年第1期44-49,共6页Yiming LI Zhufei LI Jiming YANG 
supported by the National Natural Science Foundation of China(Nos.11772325,11872356 and 11621202)。
The flow field in a typical inward-turning inlet was visualized using the Planar Laser Scattering(PLS)method in a shock tunnel with a nominal Mach number of 6.The opaque inlet,which is truncated at a series of section...
关键词：Counter-rotating Vortex Pair(CVP) Flow visualization Inward-turning inlet Planar Laser Scattering(PLS)method Shock wave 
Design method with controllable velocity direction at throat for inward-turning inlets被引量：4
《Chinese Journal of Aeronautics》2019年第6期1403-1415,共13页Wenyou QIAO Anyuan YU Wei GAO Weixing WANG 
supported by the National Natural Science Foundation of China (Nos. 11702229, 11602207 and 91641103)
In the design of a hypersonic inward-turning inlet by applying the traditional basic flowfield, a reflected shock-wave is formed in the isolator due to the continuous reflection of the cowlreflected shock wave in the ...
关键词：HYPERSONIC Inverse design Inward-turning INLET Method of characteristic Shock wave 
Aerodynamic configuration integration design of hypersonic cruise aircraft with inward-turning inlets被引量：5
《Chinese Journal of Aeronautics》2017年第4期1349-1362,共14页Jifei WANG Jinsheng CAI Chuanzhen LIU Yanhui DUAN Yaojie YU 
supported by the ‘‘111" Project of China (No. B17037)
In this work, a novel airframe/propulsion integration design method of the wing-body configuration for hypersonic cruise aircraft is proposed, where the configuration is integrated with inward-turning inlets. With the...
关键词：Aerodynamic configurations Hypersonic Integration design Inward-turning inlet Numerical simulation 
Design and experimental study of a practical Osculating Inward Cone Waverider Inlet被引量：9
《Chinese Journal of Aeronautics》2016年第6期1582-1590,共9页He Xuzhao Zhou Zheng Qin Si Wei Feng Le Jialing 
supported by the National Natural Science Foundation of China (Nos. 51376192 and 91216303)
A design method based on tip to tail streamline tracing and osculating inward cone methods is discussed for designing the integrated Osculating Inward Cone Waverider Inlet（OICWI）. A practical geometrical constrained...
关键词：INLET Integration design Inward turning cone WAVERIDER Wind tunnel experiment 
A parameterized geometry design method for inward turning inlet compatible waverider被引量：5
《Chinese Journal of Aeronautics》2013年第5期1135-1146,共12页Tian Chao Li Ni Gong Guanghong Su Zeya 
supported by the National Natural Science Foundation of China (Grant No.61004089)
Intensive studies have been carried out on generations of waverider geometry and hypersonic inlet geometry. However, integration efforts of waverider and related air-intake system are restricted majorly around the X43...
关键词：Hypersonic inlets Hypersonic vehicles Inward turning inlet Optimization PARAMETERIZATION WAVERIDER 
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