Estimates of longitudinal and lateral stability and control characteristics of Pushpak Aircraft

Varute, PT (1986) Estimates of longitudinal and lateral stability and control characteristics of Pushpak Aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    This document provides the stability and control derivatives data for the indigenously built light aircraft quot;Pushpakquot;. Analytical prediction of the aircraft modes, as well as Bode plots in frequency domain are presented.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Stability derivatives;Control derivatives;Light aircraft design data;Aircraft modes/Responses
    Subjects: AERONAUTICS > Aircraft Stability and Control
    Division/Department: Systems Engineering Division
    Depositing User: Mr. Ravikumar R
    Date Deposited: 22 Jul 2006
    Last Modified: 24 May 2010 09:47
    URI: http://nal-ir.nal.res.in/id/eprint/2314

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