Aerodynamics of delta wing-body Combinations at high angles of attack - A project proposal

Viswanath , PR (1985) Aerodynamics of delta wing-body Combinations at high angles of attack - A project proposal. Project Report. National Aerospace Laboratories, Bangalore.

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    Abstract

    Aerodynamics of highly swept wing-body configurations are dominated by vortex flows at high angles of attack . This research is proposed with a view to improving our general understanding on the nature of the vortical interactions on delta wing-body combinations and to provide information on static aerodynamic characteristics at high angles of attack. Experiments are proposed on two delta wing-body configurations at subsonic speeds. It is hoped that the results obtained from this investigation will be useful in the preliminary design of combat aircraft of the future.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: High angle of attack aerodynamics;Delta wings
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: Smt Bhagya Rekha KA
    Date Deposited: 26 Sep 2012 14:09
    Last Modified: 26 Sep 2012 14:09
    URI: http://nal-ir.nal.res.in/id/eprint/11024

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