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The Effect of Cross Flow on Slat Noise
Author(s) -
David P. Lockard,
Meelan M. Choudhari
Publication year - 2010
Publication title -
28th aiaa/ceas aeroacoustics 2022 conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2010-3835
Subject(s) - reynolds number , airfoil , flow (mathematics) , mach number , noise (video) , lift (data mining) , mechanics , cove , turbulence , physics , acoustics , computer science , geology , artificial intelligence , image (mathematics) , geomorphology , data mining
This paper continues the computational examination (AIAA Journal, Vol. 45, No. 9, 2007, pp. 2174-2186) of the unsteady flow within the slat cove region of a multi-element high-lift airfoil configuration. Two simulations have been performed to examine the effect of cross flow on the near-field fluctuations and far-field acoustics. The cross flow was imposed by changing the free-stream velocity vector and modifying the Reynolds number. The cross flow does appear to alter the dynamics in the cove region, but the impact on the noise seems to be more dependent on the flow conditions. However, separating out the true effects of the cross flow from those of the Mach and Reynolds number would require additional calculations to isolate those effects.

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