Computation of viscus transonic flow over airfoils comparisons and compilation of results

Singh, JP (1983) Computation of viscus transonic flow over airfoils comparisons and compilation of results. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    This report gives a collection of several computations13; made on NACA 0012 and NPL 9615 airfoils using a two- dimensional viscous transonic flow analysis based on Bavitz code. The comparisons with experimental results of NPL and NAL indicate that the computer program can be used as a reliable method to compute two-dimensional viscous transonic flows, except in those cases involving strong shock/extensive flow separation.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Viscous transonic flow;Airfoils;Computations
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: Poornima Narayana
    Date Deposited: 06 Sep 2006
    Last Modified: 24 May 2010 09:49
    URI: http://nal-ir.nal.res.in/id/eprint/2547

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