Dynamic Wind Tunnel Testing Of A Flexible Delta Wing

Rajamurthy, MS and Basappa, - and Bhagawan, - and Shubha, G (1993) Dynamic Wind Tunnel Testing Of A Flexible Delta Wing. Technical Report. NAL, Bangalore.

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    Abstract

    Dynamic Wind Tunnel Testing Of A Flexible Delta Wing Model W3.Carried Out To Generate Experimental Data 3To Be Used By ; The Aero-Servo-Elastic Analysis Group Of ADA . This Report Details Model Eoastruztion, Instrumentation, And Wind Tunnel Testing As Well As The Analysis Carried Out To Obtain Transfer Function As From Wind Tunnel Test Data.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Aeroservoelasticity; Flexible Delta Wing; Dynamic Wind Tunnel Testing; Time Domain Identification; Sine Sweep Tests; Acceleration Transfer Function
    Subjects: AERONAUTICS > Aeronautics (General)
    Division/Department: Systems Engineering Division, Flight Mechanics and Control Division, Systems Engineering Division, Flight Mechanics and Control Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 21 Sep 2012 10:58
    Last Modified: 21 Sep 2012 10:58
    URI: http://nal-ir.nal.res.in/id/eprint/10980

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