Approximate method of calculation of inviscid hypersonic flow

被引：0
|
作者：
Sokhanvar, F. [1 ]
Khoshnevis, A.B. [2 ]
机构：
[1] Sahand University of Technology, Iran
[2] Mechanical Engineering Dept, Sabzevar Tarbiyat Moallem University, Sabzevar, Iran
来源：
World Academy of Science, Engineering and Technology | 2009年 / 58卷
关键词：
Approximation theory - Hypersonic flow;
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摘要：
In the present work steady inviscid hypersonic flows are calculated by approximate Method. Maslens' inverse method is the chosen approximate method. For the inverse problem, parabolic shock shape is chosen for the two-dimensional flow, and the body shape and flow field are calculated using Maslen's method. For the axisymmetric inverse problem paraboloidal shock is chosen and the surface distribution of pressure is obtained.
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页码：595 / 601
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