Numerical Simulation of the Internal and External Flowfields of a Scramjet Fuel Strut Injector Including Conjugate Heat Transfer
Author:
Affiliation:
1. University of Stuttgart
2. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2207
Reference31 articles.
1. A numerical and experimental investigation of a scramjet combustor for hypersonic missile applications
2. 2Ben-Yakar, A., Kamel, M., Morris, C., Hanson, R. K. "Hypersonic Combustion and Mixing Studies using Simultaneous OH-PLIF and Schlieren Imaging,"AIAA Aerospace SciencesMeeting andExhibit, AIAA-1998-0940, 1998.
3. An experimental study of supersonic H2-AIR combustion in a shock tunnel flow facility
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