Reynolds Averaged Navier-Stokes Based Aerodynamic Analysis of Inlet for a Hypersonic Research Vehicle AIAA-2003-7067

Nair, M and Kumar, N and Saxena, S (2003) Reynolds Averaged Navier-Stokes Based Aerodynamic Analysis of Inlet for a Hypersonic Research Vehicle AIAA-2003-7067. In: 12th AIAA International Space Planes and Hypersonic Systems and Technologies, 15 - 19 December 2003, Norfolk, Virginia.

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    Abstract

    The aim of the present work is to carry out RANS computations of xB0;ow13; through the inlet of a Hypersonic Research Vehicle (HRV) with a view to ac-13; complish detailed aerodynamic analysis, which should lead to an improved design13; of the inlet. Three inlet conxAF;gurations which dixAE;er in the inlet-duct height are13; considered in this study. The results of this study are presented in the form of13; detailed computational xB0;ow visualization through density contours, variation of13; xB0;ow parameters at various desired sections and inlet performance in each case.

    Item Type: Conference or Workshop Item (Paper)
    Uncontrolled Keywords: Numerical Flow Visualization;Reynolds Averaged Naviewr-Stokes Method;Hypersonic Vehicles;Hypersonic Inlets;Aerodynamic 13; Configurations;Aerodynamicsnavier-Stokes Equationflow Visualizationcomputational Fluid Dynamics13; 13;
    Subjects: AERONAUTICS > Aeronautics (General)
    Division/Department: Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division
    Depositing User: Mr. N A
    Date Deposited: 28 Jan 2006
    Last Modified: 24 May 2010 09:40
    URI: http://nal-ir.nal.res.in/id/eprint/1029

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