Study of a Supersonic Combustor Employing Swept Ramp Fuel Injectors
Author:
Affiliation:
1. Royal Institute of Technology, Stockholm S-100 44, Sweden
2. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
3. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.5230
Reference23 articles.
1. Low angle injection into a supersonic flow
2. Noncircular jet dynamics in supersonic combustion
3. Supersonic jet mixing enhancement by 'delta-tabs'
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