Effects of Swirl and Skew Upon Supersonic Wall Jet in Crossflow
Author:
Affiliation:
1. George Washington University, Joint Institute for Advancement of Flight Sciences, Hampton, Virginia 23681-2199
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/10.2514/2.5882
Reference16 articles.
1. Low angle injection into a supersonic flow
2. Mixing studies of helium in air at high supersonic speeds
3. Study of a Supersonic Combustor Employing Swept Ramp Fuel Injectors
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