A technique to predict the aerodynamic effects of battle damage on an aircraft's wing

A technique is developed that can be used to predict the effects of battle damage on the aerodynamic performance of an aircraft’s wing. The technique is based on results obtained from wind tunnel tests on a NASA LS(1)-0417MOD aerofoil with simulated gunfire damage. The wind tunnel model incorporated...

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Bibliographic Details

Main Authors:	T.W. Pickhaver, Peter Render
Format:	Default Article
Published:	2016
Subjects:	Other engineering not elsewhere classified untagged Engineering not elsewhere classified
Online Access:	https://hdl.handle.net/2134/17506
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