RANS-based Multi-Scale Simulations of a Scramjet Combustor
Author:
Affiliation:
1. Air Force Research Laboratory
2. Japan Aerospace Exploration Agency (JAXA)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0576
Reference44 articles.
1. Numerical study of jet injection into a supersonic crossflow
2. Zonal Two Equation k-w Turbulence Models For Aerodynamic Flows
3. Gruber, M.R., Nejad, A S., J. C. Dutton, An Experimental Investigation of Transverse Injection from Circular and Elliptical Nozzles into supersonic Crossflow. Wright Lab Technical Report, 1996. WL-TR-96-2102.
4. Large structure convection velocity measurements in compressible transverse injection flowfields
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3. Analysis of Combustion Closure Assumptions in a Dual-Mode Scramjet Combustor;54th AIAA Aerospace Sciences Meeting;2016-01-02
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