Development and Critical Assessment of Technology for Numerical Simulation of Hypersonic Real Gas Flows

Saxena, SK and Nair, Manoj T (2004) Development and Critical Assessment of Technology for Numerical Simulation of Hypersonic Real Gas Flows. Project Report. National Aerospace Laboratories, Bangalore, India.

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    Abstract

    This paper provides details of the Reynolds Averaged Navier-Stokes (RANS) equations based Computational Fluid Dynamics (CFD) technology developed for numerical simulation of hypersonic real gas flows. Numerical and physical aspects of such a simulation are emphasized to bring out the challenges involved. Results of validation of the RANS code on a standard configuration for which experimental data is available are discussed.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Real gas, chemical non-equilibrium, hypersonic flow, RANS
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division
    Depositing User: MS Jayashree S
    Date Deposited: 24 Jan 2005
    Last Modified: 24 May 2010 09:39
    URI: http://nal-ir.nal.res.in/id/eprint/579

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