Wind tunnel tests on 1 /6th scale model of pilotless target aircraft configuration - 4

Mallikarjuna, HV (1987) Wind tunnel tests on 1 /6th scale model of pilotless target aircraft configuration - 4. Project Report. National Aerospace Laboratories, Bangalore.

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    Abstract

    Results of wind tunnel tests conducted on 1/6th scale model of Pilotless Target Aircraft Configuration-4 (modified and standard models) are presented in this report. This report contains' basic aerodynamic characteristics on the modified model and the calibration of static pressure ports on both the modified and standard models. The tests were conducted in the mach number range 0.2 to 0.9 and incidence range -5° to +12°.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Lift coefficient;Drag polar;Directional stability
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: Smt Bhagya Rekha KA
    Date Deposited: 10 Oct 2012 13:43
    Last Modified: 10 Oct 2012 13:43
    URI: http://nal-ir.nal.res.in/id/eprint/11041

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