WASET
	%0 Journal Article
	%A F. Sokhanvar and  A. B. Khoshnevis
	%D 2009
	%J International Journal of Mechanical and Mechatronics Engineering
	%B World Academy of Science, Engineering and Technology
	%I Open Science Index 34, 2009
	%T Approximate Method of Calculation of Inviscid Hypersonic Flow
	%U https://publications.waset.org/pdf/7375
	%V 34
	%X 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.
	%P 1272 - 1278