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|Title:||Aeolian tones generated by a square cylinder with a detached flat plate|
|Citation:||17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference), 2011, pp.1-20|
|Publisher:||American Institute of Aeronautics and Astronautics|
|Conference Name:||17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference) (5 Jun 2011 - 8 Jun 2011 : Portland, Oregon)|
|Mohamed Sukri Mat Ali, Con J. Doolan, Vincent Wheatley|
|Abstract:||The case of a rigid flat plate placed in the wake of a square cylinder for passive sound control is investigated numerically at a Reynolds number of 150 and a Mach number of 0.2. Two flow regimes are observed and these are shown to affect the radiated sound. An overall sound reduction at an observer directly above the cylinder is observed for small gap distance (G) between the cylinder and plate (0 ≤ G ≤ 2.3D, where D is the cylinder height), where a 2.9 dB reduction in sound pressure level is obtained when there is no gap between the two bodies. In contrast, the emitted sound pressure level increases by at least 8.0 dB for large gap distances (2.4D ≤ G ≤ 7D). Despite this, a 6.3 dB reduction in sound pressure level is obtained due to a sound cancellation mechanism when the plate length is reduced to 0.26D and placed 5.6D downstream of the cylinder. The maximum sound reduction attainable is shown to be limited by the non-linear unsteady stall process on the plate. © 2011 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.|
|Description:||Paper number: AIAA-2011-2779|
|Rights:||Copyright © 2011 by the American Institute of Aeronautics and Astronautics, Inc.|
|Appears in Collections:||Aurora harvest 7|
Mechanical Engineering publications
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