A Study of the Dynamic Stability Characteristics of HANSA-3 Trainer Aircraft

Kannan, SM (1999) A Study of the Dynamic Stability Characteristics of HANSA-3 Trainer Aircraft. Technical Report. National Aerospace Laboratories, Bangalore,India.

Full text available as:
[img] PDF
Restricted to Archive staff only

Download (4094Kb)

    Abstract

    This report presents the results of a study of the dynamic stability characteristics of a trainer aircraft named HANSA-3 under design and prototypeproduction13; at NAL. The study has been carried out for five different flight speeds, between the minimum speed and maximum allowable speed for most-forward, normal and most-aft C.G. locations each at three altitudes, namely, sea level, 5000 ft and 10000 ft. Longitudinal and lateral stability derivatives are evaluated and the dynamic stability characteristics of the different modes of motion are computed. The aircraft is found to have highly satisfactory stability characteristics in the most13; important and critical longitudinal short period and the lateral-directional Dutch roll modes. The aircraft meets the U.S. FAR-23 stipulations for dynamic stability,13; appropriate to this class of aircraft.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Dynamics stability;Stability derivatives;Small aircraft;Theoretical estimations Abstract
    Subjects: AERONAUTICS > Aircraft Stability and Control
    Division/Department: Experimental Aerodynamics Division
    Depositing User: Mrs Manoranjitha M D
    Date Deposited: 08 May 2006
    Last Modified: 24 May 2010 09:41
    URI: http://nal-ir.nal.res.in/id/eprint/1242

    Actions (login required)

    View Item