Computational Fluid Dynamics Simulations of a GO2/GH2 Single Element Combustor
Author:
Affiliation:
1. Institute of Space Propulsion, German Aerospace Center (DLR), 74239 Hardthausen, Germany
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/10.2514/1.B35654
Reference17 articles.
1. Benchmark Wall Heat Flux Data for a GO2/GH2 Single Element Combustor
2. Validation of High-Fidelity CFD Simulations for Rocket Injector Design
3. Computational Assessment of Gaseous Reacting Flows in Single Element Injector
4. On the k-3 stagnation point anomaly
5. On mathematical modeling of turbulent combustion with special emphasis on soot formation and combustion
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