A project proposal for high angle of attack aerodynamic characteristics of wing-body combinations

Viswanath, PR (1985) A project proposal for high angle of attack aerodynamic characteristics of wing-body combinations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    Aerodynamics of highly swept wing-body configurations are13; 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 1s 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 (Technical Report)
    Uncontrolled Keywords: High angle of attack aerodynamics;Delta wings
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: Poornima Narayana
    Date Deposited: 03 Aug 2006
    Last Modified: 24 May 2010 09:46
    URI: http://nal-ir.nal.res.in/id/eprint/2256

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