Supersonic sudden-expansion flow with fluid injection - An experimental and computational study
Author:
Affiliation:
1. GE Research and Development Center, Schenectady, NY
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-389
Reference12 articles.
1. Investigation of a Reattaching Turbulent Shear Layer: Flow Over a Backward-Facing Step
2. Non-equilibrium step-stabilized combustion of hydrogen in supersonicair
3. Computational models and methods for continuous gaseous turbulent combustion
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