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Interaction of a shock with a longitudinal vortexIn this paper we study the shock/longitudinal vortex interaction problem in axisymmetric geometry. Linearized analysis for small vortex strength is performed, and compared with results from a high order axisymmetric shock-fitted Euler solution obtained for this purpose. It is confirmed that for weak vortices, predictions from linear theory agree well with results from nonlinear numerical simulations at the shock location. To handle very strong longitudinal vortices, which may ultimately break the shock, we use an axisymmetric high order essentially non-oscillatory (ENO) shock capturing scheme. Comparison of shock-captured and shock-fitted results are performed in their regions of common validity. We also study the vortex breakdown as a function of Mach number ranging from 1.3 to 10, thus extending the range of existing results. For vortex strengths above a critical value. a triple point forms on the shock and a secondary shock forms to provide the necessary deceleration so that the fluid velocity can adjust to downstream conditions at the shock.
Document ID
19960029343
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Erlebacher, Gordon
(NASA Langley Research Center Hampton,VA United States)
Hussaini, M. Y.
(Florida State Univ. Tallahassee, FL United States)
Shu, Chi-Wang
(Brown Univ. Providence, RI United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1996
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:198332
NASA-CR-198332
Rept. 96-31
Report Number: NAS 1.26:198332
Report Number: NASA-CR-198332
Report Number: Rept. 96-31
Accession Number
96N29795
Funding Number(s)
CONTRACT_GRANT: NAG 1-1145
PROJECT: RTOP 505-90-52-01
CONTRACT_GRANT: DAAH-04-94-G-0205
CONTRACT_GRANT: NSF DMS-95-00814
CONTRACT_GRANT: AF-AFSOR-95-1-0074
CONTRACT_GRANT: NAS 1-19480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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