Numerical Investigation of the Turbulent Mixing Performance of a Cantilevered Ramp Injector
Author:
Affiliation:
1. University of Toronto, Downsview, Ontario M3H 5T6, Canada
2. Honeywell Engines, Phoenix, Arizona 85072
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1824
Reference36 articles.
1. Mixing Enhancement in Supersonic Free Shear Flows
2. Hypervelocity Scramjet Mixing Enhancement
3. Advanced injection and mixing techniques for scramjet combustors
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