Detailed Simulations of Shock-Bifurcation and Ignition of an Argon-diluted Hydrogen/Oxygen Mixture in a Shock Tube-Reference-Cited by-同舟云学术

Detailed Simulations of Shock-Bifurcation and Ignition of an Argon-diluted Hydrogen/Oxygen Mixture in a Shock Tube

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Ihme Matthias¹,Sun Yong¹,Deiterding Ralf²

Affiliation:

1. University of Michigan, Ann Arbor

2. Oak Ridge National Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-538

Reference58 articles.

1. Shock-Tube Performance at Low Initial Pressure

2. Influence of diaphragm opening time on shock-tube flows

3. 3Miller, C. G. and Jones, J. J. "Incident shock wave characteristics in air, argon, carbon dioxide, and helium in a shock tube with unheated helium driver," Tech. Rep. TN D-8099, NASA Langley Research Center Hampton, 1975.

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