Aerodynamics of battle-damaged finite-aspect-ratio wings

Wind-tunnel tests have been carried out on a battle-damaged NACA 641–412 half-wing aspect ratio of 8.2. The simulated gunfire damage had a diameter of 0.2 wing chord and was located at midchord and at one of two spanwise locations. Tests were carried out at a Reynolds number of 5:5 105. Compared wit...

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Bibliographic Details

Main Authors:	Peter M. Render, Mujahid Samad-Suhaeb, Zhiyin Yang, Mahmoud Mani
Format:	Default Article
Published:	2009
Subjects:	Other engineering not elsewhere classified untagged Engineering not elsewhere classified
Online Access:	https://hdl.handle.net/2134/5809
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