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[期刊论文] 作者：Wang Chengpeng,Xue Longsheng,Tian Xuang,,
来源：Chinese Journal of Aeronautics 年份：2017
The structure and dynamics of an oblique shock train in a duct model are investigated experimentally in a hypersonic wind tunnel.Measurements of the pressure di...
[期刊论文] 作者：WANG Chengpeng,WANG Wenshuo,XUE Longsheng,XU Pei,YANG Jinfu,
来源：南京航空航天大学学报（英文版） 年份：2019
The unstarted flow field in a hypersonic inlet model at a design point of Ma 6 is studied experimentally. The time-resolved spatial flow characteristics of the...
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