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The analysis and simulation of compressible turbulenceCompressible turbulent flows at low turbulent Mach numbers are considered. Contrary to the general belief that such flows are almost incompressible (i.e., the divergence of the velocity field remains small for all times), it is shown that even if the divergence of the initial velocity field is negligibly small, it can grow rapidly on a nondimensional time scale which is the inverse of the fluctuating Mach number. An asymptotic theory which enables one to obtain a description of the flow in terms of its divergence-free and vorticity-free components has been developed to solve the initial-value problem. As a result, the various types of low Mach number turbulent regimes have been classified with respect to the initial conditions. Formulae are derived that accurately predict the level of compressibility after the initial transients have disappeared. These results are verified by extensive direct numerical simulations of isotropic turbulence.
Document ID
19910033976
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Erlebacher, Gordon
(NASA Langley Research Center Hampton, VA, United States)
Hussaini, M. Y.
(NASA Langley Research Center Hampton, VA, United States)
Sarkar, S.
(NASA Langley Research Center; Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Kreiss, H. O.
(California, University Los Angeles, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Publication Information
Publication: Theoretical and Computational Fluid Dynamics
Volume: 2
Issue: 2, 19
ISSN: 0935-4964
Subject Category
Aerodynamics
Accession Number
91A18599
Distribution Limits
Public
Copyright
Other

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