Design of a force balance calibration rig

Desikan, KS (1974) Design of a force balance calibration rig. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    Wind tunnel tests on scale models of aero-space vehicles cover a wide range of static measurements, viz, pressure distribution, force and moments. Strain gauge balances are extensively used for the measurement of forces and moments. These balances contain constraints with bonded, resistance wire strain gauges, which connected in a bridge form gives output signal voltage proportional to the load encountered by this elements.13; 13;

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Calibration;Strain gauge
    Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
    Division/Department: Aerodynamics
    Depositing User: Mrs Manoranjitha M D
    Date Deposited: 22 Aug 2006
    Last Modified: 24 May 2010 09:49
    URI: http://nal-ir.nal.res.in/id/eprint/2567

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