论文信息 - Analysis of a New Rocket-Based Combined-Cycle Engine Concept at Low Speed

Analysis of a New Rocket-Based Combined-Cycle Engine Concept at Low Speed

S. YungsterInstitute for Computational Mechanics in Propulsion, Cleveland, OhioC.J. TrefnyGlenn Research Center, Cleveland, OhioPrepared for the35th Joint Propulsion Conference and Exhibitcosponsored by AIAA, ASME, SAE, and ASEELos Angeles, California, June 20-24, 1999Prepared under Cooperative Agreement NCC3-542National Aeronautics andSpace AdministrationGlenn Research Center

C. J. Trefny | S. Yungster

[1] P. Dimotakis. Turbulent Free Shear Layer Mixing and Combustion , 1991 .

[2] Charles J. Trefny,et al. An Air-Breathing Launch Vehicle Concept for Single-Stage-to-Orbit , 1999 .

[3] Adam P. Bruckner,et al. Numerical simulation of hypervelocity projectiles in detonable gases , 1991 .

[4] Sanford Gordon,et al. Computer program for calculation of complex chemical equilibrium compositions , 1972 .

[5] H. C. Yee. Upwind and Symmetric Shock-Capturing Schemes , 1987 .