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.
[1] S.H. Maslen, "Inviscid hypersonic flow blunt past smooth Symmetric
bodies", AIAA Journal. Vol. 2, 9 No. 6 June 1964, PP 1055-1061.
[2] J.D. Anderson, "'Hypersonic and High temperature Gas Dynamic"' ,
MacGraw Hill book Co. 1989
[3] C. F.McNeil, "Approximate Viscose Shock Layer Technique for
Calculating Hypersonic Flow About blunt-nosed Bodies", Vol. 31, No. 4 July-
August 1994, pp. 621-629.
[4] J.R. Christopher, "An approximate method for calculating threedimensional
inviscid hypersonic flow field", NASA Technical paper 3018.
[5] V.D. Milton, "Perfureation Method In Fluid Mechanich", 1964
[6] M.D. Van Dyke, , "The supersonic blunt - body problem - review and
extension" , Journal of the Aero/Space Sciences, Vol. 25, August 1958, PP.
485-495
[7] G. Morrti, and M. Abbett, "7 Time dependent computational method for
bluntbody flow ",AIAA Journal Vol., No. 12 1966, PP. 20136-2141
[8] J.D. Anderson, "Fundamental of Aerodynamics", 1988
[1] S.H. Maslen, "Inviscid hypersonic flow blunt past smooth Symmetric
bodies", AIAA Journal. Vol. 2, 9 No. 6 June 1964, PP 1055-1061.
[2] J.D. Anderson, "'Hypersonic and High temperature Gas Dynamic"' ,
MacGraw Hill book Co. 1989
[3] C. F.McNeil, "Approximate Viscose Shock Layer Technique for
Calculating Hypersonic Flow About blunt-nosed Bodies", Vol. 31, No. 4 July-
August 1994, pp. 621-629.
[4] J.R. Christopher, "An approximate method for calculating threedimensional
inviscid hypersonic flow field", NASA Technical paper 3018.
[5] V.D. Milton, "Perfureation Method In Fluid Mechanich", 1964
[6] M.D. Van Dyke, , "The supersonic blunt - body problem - review and
extension" , Journal of the Aero/Space Sciences, Vol. 25, August 1958, PP.
485-495
[7] G. Morrti, and M. Abbett, "7 Time dependent computational method for
bluntbody flow ",AIAA Journal Vol., No. 12 1966, PP. 20136-2141
[8] J.D. Anderson, "Fundamental of Aerodynamics", 1988
@article{"International Journal of Mechanical, Industrial and Aerospace Sciences:56454", author = "F. Sokhanvar and A. B. Khoshnevis", title = "Approximate Method of Calculation of Inviscid Hypersonic Flow", abstract = "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.", keywords = "Hypersonic flow, Inverse problem method", volume = "3", number = "10", pages = "1258-7", }