Preliminary results of the computation of pressure distribution on a super critical aerofoil

Sinha, UN and Ramaswamy, MA (1974) Preliminary results of the computation of pressure distribution on a super critical aerofoil. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    The preliminary results of the computation of the pressure distribution with shocks on a supercritical aerofoil using the Gerabedian and Korn's program modified to suit the IBM 370/155 Computer at Indian Institute of Technology, Madras have been reported showing the effect of the number of iterations on the result and the oomparison of the present results with that obtained by Garabedian and Korn.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Supercritical aerofoil;Transonic flow field13;
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 28 Aug 2006
    Last Modified: 24 May 2010 09:49
    URI: http://nal-ir.nal.res.in/id/eprint/2585

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