Calculation of vortex flow on a delta wing

Kumar, A and Sudharsan, R (1993) Calculation of vortex flow on a delta wing. Technical Report. National Aerospace Laboratories, Bangalore, India.

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    Solutions of Eul er equations for flow over a sharp leading-edge delta wing are presented for angles of incidence upto 46 degree using a conventional H-0 grid and a multi-block grid consisting of an inner block of conical grid covered by an outer block of H-0 grid, and computed solutions on two grids are compared . The multi -block grid i s expected to provide a better resolution of the vorti cal flow near the apex due to conical nature of the surrounding grid .

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Euler equations;Multi-block grid
    Subjects: ENGINEERING > Fluid Mechanics and Thermodynamics
    ASTRONAUTICS > Astrodynamics
    Division/Department: Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division
    Depositing User: Mrs Neetu Chandra
    Date Deposited: 10 Jul 2006
    Last Modified: 24 May 2010 09:43

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