The influence of hole orientation on the aerodynamics of battle damaged wings

Wind tunnel tests were carried out on an NASA LS(1)-0417MOD aerofoil with a circular hole simulating gunfire damage. To represent different attack directions, the inclination of the hole axis relative to the aerofoil chord was varied. The hole had a diameter of 20% of the aerofoil chord and its axis...

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Bibliographic Details
Main Authors: Peter Render, T.W. Pickhaver
Format: Default Conference proceeding
Published: 2012
Subjects:
Other engineering not elsewhere classified
Battle damage
Wing aerodynamics
Engineering not elsewhere classified
Online Access:https://hdl.handle.net/2134/10067
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https://hdl.handle.net/2134/10067

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