An assumed joint-Beta PDF approach for supersonic turbulent combustion
Author:
Affiliation:
1. North Carolina StateUniversity, Raleigh
2. NASA, Langley Research Center,Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3844
Reference11 articles.
1. Finite-rate chemistry effects in a Mach 2 reacting flow
2. Turbulent flows with nonpremixed reactants
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4. A two-variables formalism for the treatment of chemical reactions in turbulent H2—Air diffusion flames
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