Estimation of the longitudinal stability characterisiticvs of MIG 21BIS Aircraft from Flight DATA

Srinathkumar, S and Parameswaran, V and Girija, G (1986) Estimation of the longitudinal stability characterisiticvs of MIG 21BIS Aircraft from Flight DATA. Project Report. National Aerospace Laboratories, Bangalore.

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    Abstract

    This report presents the parameter estimation results derived from flight test data of a MIG-21BIS aircraft . The flight test program was executed by Aircraft & Systems Testing establishment (ASTE) and the flight data analysis was carried out at NAL . The aircraft was tested in four configurations to evaluate the effect of i) a vortex plate attached to the leading edge of the wing to improve the drag characteristics and ii) a larger saddle tank to improve the range.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Flight Test, Parameter Estimation, Stability derivatives
    Subjects: AERONAUTICS > Aircraft Stability and Control
    Division/Department: Flight Mechanics and Control Division, Flight Mechanics and Control Division, Systems Engineering Division
    Depositing User: Ms Indrani V
    Date Deposited: 12 Oct 2012 14:01
    Last Modified: 12 Oct 2012 14:01
    URI: http://nal-ir.nal.res.in/id/eprint/11087

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