Publisher
American Institute of Aeronautics and Astronautics
Reference14 articles.
1. O. Knab, A. Froehlich and D. Wennerberg, "Design Support for Advanced Storable Propellant Engines by ROCFLAMAnalysis,"AIAA99-2459,1999
2. B.R. Lawver,HighPerformanceN2O4/AMINEElements"Blowapart",NASACR-160273,1979
3. J. H. Rupe, "An Experimental Correlation of the Non-reactive Properties of Injection Schemes and Combustion EffectsinaLiquid-PropellantRocketEngine,PartI.TheApplicationofNon-reactiveSprayPropertiestoRocket-MotorInjector Design,"Jet PropulsionLaboratory TechnicalReportNo.32-255,1965
4. X. Li, M. Arienti, M. C. Soteriou and M. Sussman, "Towards an Efficient, High-Fidelity Methodology for Liquid JetAtomizationComputations,"AIAApaper2010-0210,2010
5. M. Arienti, X. Li, M. C. Soteriou and C. A. Eckett, "Coupled Level-Set/Volume-of-Fluid Method for the SimulationofLiquidAtomization inPropulsionDeviceInjectors,"AIAApaper2010-7136