Evaluation of parallel injector configurations for Mach 2 combustion
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23665
2. George Washington University, Hampton, Virginia 23665
3. Analytical Services and Materials, Hampton, Virginia 23665
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/10.2514/3.23503
Reference13 articles.
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