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Computation of Sound Generated by Viscous Flow Over a Circular CylinderThe Lighthill acoustic analogy approach combined with Reynolds-averaged Navier Stokes is used to predict the sound generated by unsteady viscous flow past a circular cylinder assuming a correlation length of 10 cylinder diameters. The two-dimensional unsteady flow field is computed using two Navier-Stokes codes at a low Mach number over a range of Reynolds numbers from 100 to 5 million. Both laminar flow as well as turbulent flow with a variety of eddy viscosity turbulence models are employed. Mean drag and Strouhal number are examined, and trends similar to experiments are observed. Computing the noise within the Reynolds number regime where transition to turbulence occurs near the separation point is problematic: laminar flow exhibits chaotic behavior and turbulent flow exhibits strong dependence on the turbulence model employed. Comparisons of far-field noise with experiment at a Reynolds number of 90,000, therefore, vary significantly, depending on the turbulence model. At a high Reynolds number outside this regime, three different turbulence models yield self-consistent results.
Document ID
19970017057
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Cox, Jared S.
(George Washington Univ. Hampton, VA United States)
Rumsey, Christopher L.
(NASA Langley Research Center Hampton, VA United States)
Brentner, Kenneth S.
(NASA Langley Research Center Hampton, VA United States)
Younis, Bassam A.
(City Univ. London, United Kingdom)
Date Acquired
September 6, 2013
Publication Date
March 1, 1997
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:110339
NASA-TM-110339
Accession Number
97N19417
Funding Number(s)
PROJECT: RTOP 533-31-21-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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