Instrumentation for ASE Experiments in the Dynamic Wind Tunnel

Poornima, L and Seshadri, K (1991) Instrumentation for ASE Experiments in the Dynamic Wind Tunnel. Technical Report. National Aerospace Laboratories, Bangalore, India.

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    Abstract

    The instrumentation package developed for use with the13; flexible wing models to be tested in the dynamic wind tunnel for aero-servo-elastic studies is detailed.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Strain gauge amplifiers;Servo drive;Aero-servo-elasticity
    Subjects: AERONAUTICS > Avionics & Aircraft Instrumentation
    Division/Department: Other, Flight Mechanics and Control Division
    Depositing User: Mr. Ravikumar R
    Date Deposited: 23 Jun 2006
    Last Modified: 24 May 2010 09:43
    URI: http://nal-ir.nal.res.in/id/eprint/1791

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