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Acoustics and Surface Pressure Measurements from Tandem Cylinder ConfigurationsAcoustic and unsteady surface pressure measurements from two cylinders in tandem configurations were acquired to study the effect of spacing, surface trip and freestream velocity on the radiated noise. The Reynolds number ranged from 1.15x10(exp 5) to 2.17x10(exp 5), and the cylinder spacing varied between 1.435 and 3.7 cylinder diameters. The acoustic and surface pressure spectral characteristics associated with the different flow regimes produced by the cylinders' wake interference were identified. The dependence of the Strouhal number, peak Sound Pressure Level and spanwise coherence on cylinder spacing and flow velocity was examined. Directivity measurements were performed to determine how well the dipole assumption for the radiation of vortex shedding noise holds for the largest and smallest cylinder spacing tested.
Document ID
20140010019
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Hutcheson, Florence V.
(NASA Langley Research Center Hampton, VA, United States)
Brooks, Thomas F.
(NASA Langley Research Center Hampton, VA, United States)
Lockard, David P.
(NASA Langley Research Center Hampton, VA, United States)
Choudhari, Meelan M.
(NASA Langley Research Center Hampton, VA, United States)
Stead, Daniel J.
(Northrop Grumman Corp. Hampton, VA, United States)
Date Acquired
July 23, 2014
Publication Date
June 8, 2014
Subject Category
Acoustics
Report/Patent Number
AIAA Paper 2014-2762
NF1676L-17625
Meeting Information
Meeting: AIAA/CEAS Aeroacoustics Conference
Location: Atlanta, GA
Country: United States
Start Date: June 17, 2014
End Date: June 20, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 699959.02.07.07.08
Distribution Limits
Public
Copyright
Public Use Permitted.
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