Priliminary results of the computation of pressure distribution on a supercritical aerofoil

Sinha, UN and Ramaswamy, MA (1974) Priliminary results of the computation of pressure distribution on a supercritical 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 the13; result and the comparison of the present results with that obtained by Garabedian and Korn.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Aerofoil
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 30 Aug 2006
    Last Modified: 24 May 2010 09:49
    URI: http://nal-ir.nal.res.in/id/eprint/2584

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