Contributions by NAL Aerodynamics Division at SLV-3 Review

Rao, DM and Rajendra, G and Sundaramurthy, H and Kanagarajan, V (1975) Contributions by NAL Aerodynamics Division at SLV-3 Review. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    A 16 mm black-and-white motion picture was taken through the13; Schlieren system of the 4-ft. tunnel during supersonic tests of13; the SLV-3 Booster model. The purpose was to record the observed13; sudden changes in the configuration of the lee-ward vortices on13; the booster model at higher angles of attack, which appeared to13; coincide with abrupt reversals of the side force measured simultaneously on the balance13;

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: SLV-3;High-angle of attack;4ft tunnel;Wind tunnel
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics, Aerodynamics, Aerodynamics
    Depositing User: Mrs Manoranjitha M D
    Date Deposited: 22 Aug 2006
    Last Modified: 24 May 2010 09:49

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