A two–step kinetics model for numerical simulation of explosions and detonations in H 2

A two–step kinetics model for numerical simulation of explosions and detonations in H 2 –O 2 mixtures

Published:2002-01-08 Issue:2017 Volume:458 Page:49-82
ISSN:1364-5021
Container-title:Proceedings of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences
language:en
Short-container-title:Proc. R. Soc. Lond. A

Author:

Sichel M.¹,Tonello N. A.²,Oran E. S.³,Jones D. A.⁴

Affiliation:

1. Department of Aerospace Engineering, The University of Michigan, Ann Arbor, MI 48109, USA ()

2. Computational Dynamics Ltd, 200 Shepherd's Bush Road, London W6 7NY, UK

3. Laboratory for Computational Physics and Fluid Dynamics, Naval Research Laboratory, Code 6404, Washington, DC 20375, USA ()

4. Aeronautical and Maritime Research Laboratory, DSTO, PO Box 4331, Victoria 3001, Australia

Publisher

The Royal Society

Subject

General Physics and Astronomy,General Engineering,General Mathematics

Link

Reference73 articles.

2. Numerical modeling of galloping detonation;Aksamentov S. M.;Prog. Aeronaut. Astronaut.,1992

3. Baulch D. L. Drysdale D. D. Horne D. G. & Lloyd A. C. 1972 Evaluated data for high temperature reactions. London: Butterworths.

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