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Non-linear interaction of a detonation/vorticity waveThe interaction of an oblique, overdriven detonation wave with a vorticity disturbance is investigated by a direct two-dimensional numerical simulation using a multi-domain, finite-difference solution of the compressible Euler equations. The results are compared to those of linear theory, which predict that the effect of exothermicity on the interaction is relatively small except possibly near a critical angle where linear theory no longer holds. It is found that the steady-state computational results agree with the results of linear theory. However, for cases with incident angle near the critical angle, moderate disturbance amplitudes, and/or sudden transient encounter with a disturbance, the effects of exothermicity are more pronounced than predicted by linear theory. Finally, it is found that linear theory correctly determines the critical angle.
Document ID
19910014121
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Lasseigne, D. G.
(Old Dominion Univ. Norfolk, VA., United States)
Jackson, T. L.
(Old Dominion Univ. Norfolk, VA., United States)
Hussaini, M. Y.
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1991
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ICASE-91-34
AD-A236501
AD-A-236501
NAS 1.26:187550
NASA-CR-187550
Report Number: ICASE-91-34
Report Number: AD-A236501
Report Number: AD-A-236501
Report Number: NAS 1.26:187550
Report Number: NASA-CR-187550
Accession Number
91N23434
Funding Number(s)
CONTRACT_GRANT: NAS1-18605
PROJECT: RTOP 505-90-52-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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