Yang, Zhiyin, Samad-Suhaeb, Mujahid and Render, Peter M (2012) Computational study of a battle damaged finite aspect ratio wing. In: 30th AIAA Applied Aerodynamics Conference, 25-28th June, New Orleans, USA.

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Abstract

Numerical studies have been carried out on a battle damaged NACA 641-412 half wing of aspect ratio 8.2 at a Reynolds number of 5.5 x 105. The simulated gunfire damage was represented by a single hole with a diameter of 0.2 wing chord. The hole was centred at half chord and at spanwise locations of 450mm and 650mm from wing root. Computational Fluid Dynamics (CFD) results have been compared with experimental data and a general overall good agreement has been obtained, in the flow features introduced by the damage. Furthermore, the flow field inside the damage hole and in the region downstream of the jet have been analysed in more detail using CFD.

Item Type:	Conference or Workshop Item (Paper)
Schools and Departments:	School of Engineering and Informatics > Engineering and Design
Subjects:	T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL0500 Aeronautics. Aeronautical engineering
Depositing User:	Zhiyin Yang
Date Deposited:	07 Aug 2012 08:26
Last Modified:	07 Aug 2012 08:26
URI:	http://sro.sussex.ac.uk/id/eprint/40249

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