Surface Pressure Estimates for Pitching Aircraft Model at High Angles-of-attack13; 13;

Pashilkar, AA (2002) Surface Pressure Estimates for Pitching Aircraft Model at High Angles-of-attack13; 13;. Defence Science Journal, 52 (4). pp. 417-427.

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    Abstract

    The surface pressure on a pitching delta wing aircraft is estimated from the normal force and the pitching moment characteristics. The pressure model is based on parametrising the surface pressure distribution on a simple delta wing. This model is useful as a first approximation of the load distribution on the aircraft wing. Leeward surface pressure distributions computed by this method are presented.

    Item Type: Journal Article
    Uncontrolled Keywords: Surface pressure;Delta wing aircraft;Aircraft wing;Load distribution;Aerodynamics;Vortex breakdown;Computational fluid dynamics;Surface pressure model;Angle-of-attack
    Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
    Division/Department: Flight Mechanics and Control Division
    Depositing User: Ms. Alphones Mary
    Date Deposited: 22 Jun 2006
    Last Modified: 24 May 2010 09:43
    URI: http://nal-ir.nal.res.in/id/eprint/1671

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