2002•Baozha yu chongjiRequires access
On Some Problems of Moving Shock Wave in the Supersonic Flow
Gang Tao
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Abstract
In this paper the moving oblique shock wave of the non viscosity perfect gas flow are studied. The influence of moving shock wave on the ratio of total enthalpy, total pressure and the turning angle of flow passing through shock wave are given and analyzed, The calculated results show obviously difference from those under stationary shock wave condition. This problem is related to the auto vibration of shock wave or abnormal heating,In the bottom of container when there is interaction between the supersonic jet and the obstruction or the container.