Flow calculation over a delta-wing using the thin-layer wavier-stokes equations

Kumar, Anand (1989) Flow calculation over a delta-wing using the thin-layer wavier-stokes equations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    A 3D laminar thin-layer Navier-Stokes solver is developed13; which employs finite volume spatial discretisation and13; Runge-Kutta time integration. The code is applied to compute vortex flow over a round leading edge delta wing, and the results are compared with experiment and an Euler simulation.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Navier-stokes equatins;Vortex flow
    Subjects: ENGINEERING > Fluid Mechanics and Thermodynamics
    Division/Department: Computational and Theoretical Fluid Dynamics Division
    Depositing User: Mr. Ravikumar R
    Date Deposited: 31 Jul 2006
    Last Modified: 24 May 2010 09:44
    URI: http://nal-ir.nal.res.in/id/eprint/1950

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