Study on Mach stems induced by interaction of planar shock waves on two intersecting wedges  被引量:6

Study on Mach stems induced by interaction of planar shock waves on two intersecting wedges

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作  者:Gaoxiang Xiang Chun Wang Honghui Teng Yang Yang Zonglin Jiang 

机构地区:[1]Institute of Mechanics, Chinese Academy of Sciences

出  处:《Acta Mechanica Sinica》2016年第3期362-368,共7页力学学报(英文版)

基  金:supported by the National Natural Science Foundation of China (Grants 11372333, 90916028)

摘  要:The properties of Mach stems in hypersonic corner flow induced by Mach interaction over 3D intersecting wedges were studied theoretically and numerically.A new method called "spatial dimension reduction" was used to analyze theoretically the location and Mach number behind Mach stems. By using this approach, the problem of 3D steady shock/shock interaction over 3D intersecting wedges was transformed into a 2D moving one on cross sections, which can be solved by shock-polar theory and shock dynamics theory. The properties of Mach interaction over 3D intersecting wedges can be analyzed with the new method,including pressure, temperature, density in the vicinity of triple points, location, and Mach number behind Mach stems.Theoretical results were compared with numerical results,and good agreement was obtained. Also, the influence of Mach number and wedge angle on the properties of a 3D Mach stem was studied.The properties of Mach stems in hypersonic corner flow induced by Mach interaction over 3D intersecting wedges were studied theoretically and numerically.A new method called "spatial dimension reduction" was used to analyze theoretically the location and Mach number behind Mach stems. By using this approach, the problem of 3D steady shock/shock interaction over 3D intersecting wedges was transformed into a 2D moving one on cross sections, which can be solved by shock-polar theory and shock dynamics theory. The properties of Mach interaction over 3D intersecting wedges can be analyzed with the new method,including pressure, temperature, density in the vicinity of triple points, location, and Mach number behind Mach stems.Theoretical results were compared with numerical results,and good agreement was obtained. Also, the influence of Mach number and wedge angle on the properties of a 3D Mach stem was studied.

关 键 词:3D shock/shock interaction Mach interaction Spatial dimension reduction 

分 类 号:O354.5[理学—流体力学]

 

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