Self-ignition and transition to flame-holding in a rectangular scramjet combustor with a backward step-Reference-Cited by-同舟云学术

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Self-ignition and transition to flame-holding in a rectangular scramjet combustor with a backward step

Published:2000-01 Issue:1 Volume:28 Page:705-712
ISSN:1540-7489
Container-title:Proceedings of the Combustion Institute
language:en
Short-container-title:Proceedings of the Combustion Institute

Author:

Takahashi Shuhei,Yamano Goro,Wakai Kazunobi,Tsue Mitsuhiro,Kono Michikata

Publisher

Elsevier BV

Subject

Physical and Theoretical Chemistry,Mechanical Engineering,General Chemical Engineering

Reference13 articles.

1. Criteria for Self-Ignition of Supersonic Hydrogen-Air Mixtures;Huber;NASA TP-1457,1979

2. Experimental supersonic hydrogen combustion employing staged injection behind a rearward-facing step

3. Mixing and Chemical Kinetics Interactions in a Mach 2 Reacting Flow

4. Effects of injector geometry on scramjet combustor performance

5. Ignition Strategy in a Model Scramjet;Tomioka,1996

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