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Numerical Simulations of High-Speed Chemically Reacting FlowThe essentially nonoscillatory (ENO) shock-capturing scheme for the solution of hyperbolic equations is extended to solve a system of coupled conservation equations governing two-dimensional, time-dependent, compressible chemically reacting flow with full chemistry. The thermodynamic properties of the mixture are modeled accurately, and stiff kinetic terms are separated from the fluid motion by a fractional step algorithm. The methodology is used to study the concept of shock-induced mixing and combustion, a process by which the interaction of a shock wave with a jet of low-density hydrogen fuel enhances mixing through streamwise vorticity generation. Test cases with and without chemical reaction are explored here. Our results indicate that, in the temperature range examined, vorticity generation as well as the distribution of atomic species do not change significantly with the introduction of a chemical reaction and subsequent heat release. The actual diffusion of hydrogen is also relatively unaffected by the reaction process. This suggests that the fluid mechanics of this problem may be successfully decoupled from the combustion processes, and that computation of the mixing problem (without combustion chemistry) can elucidate much of the important physical features of the flow.
Document ID
19970023110
Acquisition Source
Armstrong Flight Research Center
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Ton, V. T.
(California Univ. Los Angeles, CA United States)
Karagozian, A. R.
(California Univ. Los Angeles, CA United States)
Marble, F. E.
(California Univ. Los Angeles, CA United States)
Osher, S. J.
(California Univ. Los Angeles, CA United States)
Engquist, B. E.
(California Univ. Los Angeles, CA United States)
Date Acquired
August 17, 2013
Publication Date
January 1, 1994
Publication Information
Publication: Theoretical and Computational Fluid Dynamics
Publisher: Springer-Verlag G.m.b.H. and Co. K.G.
Volume: 6
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-203703
NAS 1.26:203703
Accession Number
97N72166
Funding Number(s)
CONTRACT_GRANT: NCC2-374
CONTRACT_GRANT: N00014-86-K-0691
CONTRACT_GRANT: NSF DMS-88-11863
Distribution Limits
Public
Copyright
Public Use Permitted.
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