Experimental Study on Pitch up Problem Associated with Compound Delta Wings of Combat Aircraft Configurations

Ahmed, Sajeer and Sudhakar, S (2009) Experimental Study on Pitch up Problem Associated with Compound Delta Wings of Combat Aircraft Configurations. Project Report. National Aerospace Laboratories, Bangalore.

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    Abstract

    This report highlights the progress of the work carried out in the above project including the statement of expenditure for presentation at AR&DB annual symposium-2009

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Compound delta wing, Pitch up, Subsonic speeds
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Experimental Aerodynamics Division, Experimental Aerodynamics Division
    Depositing User: Smt Bhagya Rekha KA
    Date Deposited: 20 Sep 2011 11:09
    Last Modified: 20 Sep 2011 11:09
    URI: http://nal-ir.nal.res.in/id/eprint/9964

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