On Maslen's solution for inviscid flow past blunt bodies

Gopinath, R (1966) On Maslen's solution for inviscid flow past blunt bodies. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Maslen's solution for the inviscid flow past blunt bodies at13; hypersonic speeds was investigated for the presence of singularity, if any, in the sonic region, both for equilibrium as well as non equilibrium flows. The shock stand-off distance was calculated by the above method and compared with the results available by other methods. The calculated value compared favourably with those by other methods. Also, an attempt was made to determine the shape of the shock wave for a given distribution of entropy behind the shock wave.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Maslen's solution;Inviscid flow;Blunt bodies;Hypersonic speeds;13; Equilibrium flows;Shock stand-off
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 21 Dec 2006
    Last Modified: 24 May 2010 09:54
    URI: http://nal-ir.nal.res.in/id/eprint/3692

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