CFD validation for scramjet combustor and nozzle flows. I
Author:
Affiliation:
1. Sverdrup Technology, Inc., Arnold AFB, TN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-1840
Reference19 articles.
1. An efficient two-dimensional engineering design code for scramjet combustor, nozzle, and plume analysis
2. Two and three dimensional parabolized Navier-Stokes code for scramjet combustor, nozzle, and film cooling analysis
3. A set of strongly coupled, upwind algorithms for computing flows in chemical nonequilibrium
4. Characteristic-based algorithms for flows in thermochemical nonequilibrium
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1. Advances and challenges in modeling high-speed turbulent combustion in propulsion systems;Progress in Energy and Combustion Science;2017-05
2. Scalar Fluctuation and Transport Modeling for Application to High Speed Reacting Flows;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09
3. Prediction of turbulent reacting flows related to hypersonic airbreathing propulsion systems;30th Joint Propulsion Conference and Exhibit;1994-06-27
4. Computation of high-speed turbulent reacting flows relevant to scramjet combustors;Fluid Dynamics Conference;1994-06-20
5. CFD validation and evaluation for combustor and nozzle flows. II;32nd Aerospace Sciences Meeting and Exhibit;1994-01-10
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