CAA boundary conditions for airfoil noise due to high-frequency gusts
CAA boundary conditions for airfoil noise due to high-frequency gusts
244-253
Kim, J.W.
fedabfc6-312c-40fd-b0c1-7b4a3ca80987
Lau, A.S.H
b8e01ce1-5d41-4502-bf81-213f6426b38f
Sandham, N.D.
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28 October 2010
Kim, J.W.
fedabfc6-312c-40fd-b0c1-7b4a3ca80987
Lau, A.S.H
b8e01ce1-5d41-4502-bf81-213f6426b38f
Sandham, N.D.
0024d8cd-c788-4811-a470-57934fbdcf97
Kim, J.W., Lau, A.S.H and Sandham, N.D.
(2010)
CAA boundary conditions for airfoil noise due to high-frequency gusts.
Procedia Engineering, 6 (1), .
(doi:10.1016/j.proeng.2010.09.026).
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Published date: 28 October 2010
Venue - Dates:
IUTAM Symposium on Computational Aeroacoustics for Aircraft Noise Prediction, 2010-10-28
Organisations:
Aerodynamics & Flight Mechanics
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Local EPrints ID: 166481
URI: http://eprints.soton.ac.uk/id/eprint/166481
PURE UUID: cec9a6e2-4ef9-4f00-b680-aa4b26618218
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Date deposited: 29 Oct 2010 07:56
Last modified: 14 Mar 2024 02:49
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Author:
A.S.H Lau
Author:
N.D. Sandham
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