Rocket Combustion Modelling Test Case RCM-3. Numerical Calculation of MASCOTTE 60 bar Case with THESEE
SOCIETY NATIONAL D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION MOISSY-CRAMAYEL (FRANCE)
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This paper presents the numerical simulation of the RCM-3 test case done by Snecma and LCSR. The specified inlet conditions and computational options are described in the paper. A brief discussion about the main results is also given.
- Computer Programming and Software
- Combustion and Ignition