Analysis of Mixing Enhancement Using Streamwise Vortices in a Supersonic Combustor by Application of Laser Diagnostics
Author:
Affiliation:
1. National Aerospace Laboratory
2. DLR Lampoldshausen
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-5203
Reference42 articles.
1. Mixing-Controlled Supersonic Combustion
2. Mixing Enhancement in Supersonic Free Shear Flows
3. Compressibility Effects in Turbulent Shear Layers
4. The compressible turbulent shear layer: an experimental study
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