TY - JFULL AU - F. Sokhanvar and A. B. Khoshnevis PY - 2009/11/ TI - Approximate Method of Calculation of Inviscid Hypersonic Flow T2 - International Journal of Mechanical and Mechatronics Engineering SP - 1271 EP - 1278 VL - 3 SN - 1307-6892 UR - https://publications.waset.org/pdf/7375 PU - World Academy of Science, Engineering and Technology NX - Open Science Index 34, 2009 N2 - 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. ER -