Approximate Method of Calculation of Inviscid Hypersonic Flow

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.

Authors:

• F. Sokhanvar
• A. B. Khoshnevis

Keywords:

• Hypersonic flow
• Inverse problem method

References:

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