Computational fluid dynamics prediction of the reacting flowfield inside a subscale scramjet combustor
Author:
Affiliation:
1. ViGYAN, Inc., Hampton, Virginia 23665
2. NASA Langley Research Center, 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/10.2514/3.23292
Reference5 articles.
1. Using a global hydrogen-air combustion model in turbulent reacting flow calculations
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3. Numerical simulation of angular injection of hydrogen fuel in scramjet combustor;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2011-09-26
4. Numerical Simulation of Supersonic Combustion with Parallel Injection of Hydrogen Fuel;Defence Science Journal;2010-07-23
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