Slope and deflection of 4-FT.Tunnel model support stings

Desikan, KS (1972) Slope and deflection of 4-FT.Tunnel model support stings. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    The models for force and pressure measurements in 4-ft. Trisonic Wind Tunnel are generally mounted on stings. For pressure measurements, the model is directly secured on to the sting and for force measurements, the model is supported via a balance mounted on the stings.13;

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Trisonic wind tunnel;Pressure measurements
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 10 Nov 2006
    Last Modified: 24 May 2010 09:53

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