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: Monograph (Technical Report)
Uncontrolled Keywords: Stability derivatives;Control derivatives;Light aircraft design data;Aircraft modes/Responses
Subjects: AERONAUTICS > Aircraft Stability and Control
Depositing User: Mr. Ravikumar R
Date Deposited: 22 Jul 2006
Last Modified: 24 May 2010 04:17
URI: http://nal-ir.nal.res.in/id/eprint/2314

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