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CFD Simulation on the J-2X Engine Exhaust in The Center-Body Diffuser and Spray Chamber at the B-2 Facility

机译:B-2设施中心体扩散器和喷雾室中J-2X发动机排气的CFD模拟

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A computational fluid dynamic (CFD) code is used to simulate the J-2X engine exhaust in the centerbody diffuser and spray chamber at the Spacecraft Propulsion Facility (B-2). The CFD code is named as the space-time conservation element and solution element (CESE) Euler solver and is very robust at shock capturing. The CESE results are compared with independent analysis results obtained by using the National Combustion Code (NCC) and show excellent agreement.

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