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Turbulence alteration due to shock motionPhysical and computational models are provided for three cases of shock motion-turbulence interaction: (1) the production of velocity fluctuations due to shock oscillations; (2) eddy alteration due to transient eddy shocklets; and (3) eddy production due to transient shock-entropy spottiness interactions. Shock motions are shown to be efficient in converting mean flow energy into fluctuation energy, and high-frequency induced shock motions produce intense vorticity fields from the incident mean flow. The effects of transient eddy shocklets created by subsonic eddy motion in a supersonic stream are discussed in detail.
Document ID
19880063949
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hussaini, M. Y.
(NASA Langley Research Center Institute for Computer Applications in Science and Engineering, Hampton, VA, United States)
Collier, F.
(Virginia Polytechnic Institute and State University Blacksburg, United States)
Bushnell, D. M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Aerodynamics
Accession Number
88A51176
Funding Number(s)
CONTRACT_GRANT: NAS1-17170
Distribution Limits
Public
Copyright
Other

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