Moment stability Derivatives of N A G Missile Configuration-at Low Speed using Semi-free Dynamic Flying

Balakrishna, S and Niranjana, T and Rajan, SR Moment stability Derivatives of N A G Missile Configuration-at Low Speed using Semi-free Dynamic Flying. Project Report. NAL, Bangalore.

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    Abstract

    Dynamic flying of scaled model exploits the advantages of flight test methodology and wind tunnel flexibility to generate stability derivative data in evaluated using dynamic flying A 1 : 1 .45 scaled model is flown in a low speed, tunnel and its pitching response to servoed tail drive doublet is analysed using Maximum Likelihood Estimation method . The results indicate a low angle of attack static instability for the tested configuration.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Dynamic Flying;Stability Derivatives
    Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
    Division/Department: Systems Engineering Division, Systems Engineering Division, Systems Engineering Division
    Depositing User: Mr Nisanth
    Date Deposited: 17 Jul 2012 10:41
    Last Modified: 17 Jul 2012 10:41
    URI: http://nal-ir.nal.res.in/id/eprint/10582

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