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The Boundary Layer Interaction with Shock Wave and Expansion Fan

The Boundary Layer Interaction with Shock Wave and Expansion Fan

作     者:Marat A. Goldfeld Roman V. Nestoulia Alexei V. Starov Institute of Theoretical and Applied Mechanics, 4/1, Institutskaya Str., Novosibirsk 630090, Russia. 

作者机构:Institute of Theoretical and Applied Mechanics Novosibirsk Russia 

出 版 物:《Journal of Thermal Science》 (热科学学报(英文版))

年 卷 期:2000年第9卷第2期

页      面:109-114页

核心收录:

学科分类:080701[工学-工程热物理] 08[工学] 0807[工学-动力工程及工程热物理] 

主  题:boundary layer shock wave expansion fan relaxation separation. 

摘      要:The results of experimental investigation of a turbulent boundary layer on compression and expansion surfaces are presented. They include the study of the shock wave and/or expansion fan action upon the boundary layer, boundary layer separation and its relaxation. Complex events of paired interactions and the flow on compression convex-concave surfaces were studied. The possibility and conditions of the boundary layer relaminarization behind the expansion fan and its effect on the relaxation length are presented. Different model configurations for wide range conditions were investigated. Comparison of results for different interactions was carried out.

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