Validation of a NASA code for determining the viscous supersonic flow past a pointed body of revolution

Dutta, Vimala and Ramamoorthy, P (1988) Validation of a NASA code for determining the viscous supersonic flow past a pointed body of revolution. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    An existing NASA Code is validated on UNIVAC mining . the supersonic flow-past a pointed body 1100/71 for deterof revolution at zero incidence with a fully turbulent boundary layer. The programme geometry in any systerTi is suitably modified to allow the Input of body of units. Results for the test case of RM-10 body obtained by the NAL code and the original NASA code totally agree. Inviscid pressure13; by using this code are distributions on two bomb models obtained compared with those of Woodward's programme .

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Supersonic flow;Body of revolution
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Fluid Dynamics, Fluid Dynamics
    Depositing User: Poornima Narayana
    Date Deposited: 11 Aug 2006
    Last Modified: 24 May 2010 09:45
    URI: http://nal-ir.nal.res.in/id/eprint/2023

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