Numerical Simulation of Ethylene Injection from In-stream Fueling Pylons
Author:
Affiliation:
1. Air Force Institute of Technology
2. U.S. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2518
Reference9 articles.
1. Pylon Fuel Injector Design for a Scramjet Combustor
2. Evaluation of parallel injector configurations for supersonic combustion
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4. Mixing and combustion in scramjet combustor with raised and relieved ramp
5. Analysis of Mixing Enhancement Using Streamwise Vortices in a Supersonic Combustor by Application of Laser Diagnostics
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