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On the interaction of a sound pulse with the shear layer of an axisymmetric jet. Part 3: Nonlinear effectsThe fluctuating field of a jet excited by transient mass injection is simulated numerically. The model is developed by expanding the state vector as a mean state plus a fluctuating state. Nonlinear terms are not neglected, and the effect of nonlinearity was studied. A high order numerical method is used to compute the solution. The results show a significant spectral broadening in the flow field due to the nonlinearity. In addition, large scale structures are broken down into smaller scales.
Document ID
19850010354
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bayliss, A.
(Exxon Corp. Research Clinton, N.J., United States)
Maestrello, L.
(NASA Langley Research Center Hampton, VA, United States)
Turkel, E.
(Tel Aviv Univ.)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Acoustics
Report/Patent Number
ICASE-84-61
NASA-CR-172512
NAS 1.26:172512
Report Number: ICASE-84-61
Report Number: NASA-CR-172512
Report Number: NAS 1.26:172512
Accession Number
85N18663
Funding Number(s)
CONTRACT_GRANT: NAS1-17130
CONTRACT_GRANT: NAS1-15810
CONTRACT_GRANT: NAS1-17170
CONTRACT_GRANT: NAS1-16394
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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