Dynamic flying investigations on 1/13.5 NALLA Model (Longitudinal Results)

Balakrishna, S and Niranjana, T and Rajan, SR and Rajamurthy, MS (1991) Dynamic flying investigations on 1/13.5 NALLA Model (Longitudinal Results). Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    A 1/13.5 Scale NALLA model has been instrumented and13; dynamcally flown with one degree of freedom. Experiments13; have been conducted at CG locations of 0.28 C amp; 0.43 C13; The Neutral point of the configuration has been shown13; to be in the range 0.57 C to 0.58 C suggesting - aft13; loading. The power effect is shown to be pitch up above13; 10xB0; alpha trim and pitch down below 10xB0; alpha.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Dynamic flying investigations;Longitudinal results;Stability and control;Neural point
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 10 Oct 2006
    Last Modified: 24 May 2010 09:51
    URI: http://nal-ir.nal.res.in/id/eprint/2941

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