Impact of Axial Vortices on Mixing at a High Convective Mach Number
Author:
Affiliation:
1. University of Toronto Institute for Aerospace Studies, Downsview, Ontario M3H 5T6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2086
Reference13 articles.
1. Investigation of a contoured wall injector for hypervelocity mixing augmentation
2. A comparative study of hypersonic fuel/air mixing enhancement by ramp and cantilevered ramp injectors
3. Numerical Investigation of the Turbulent Mixing Performance of a Cantilevered Ramp Injector
4. Numerical Simulation of Hypersonic Shock-Induced Combustion Ramjets
5. An experimental study of the effect of streamwise vorticity on supersonic mixing enhancement
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