Progress in Propulsion Physics · 2016 · 13 citations · 8 references
EngineeringChemical EngineeringMechanical EngineeringCombustionComputational Heat TransferHeat TransferCombustion FundamentalsCombustion KineticsCombustion ProcessesCombustion Reaction EngineeringCooling SystemsHeat Transfer ModelingCombustion Chamber DesignCombustion Chamber Heat TransferCoolingFilm CoolingFinite-rate Chemistry ModelingHeat Flux ModelingMethaneWall Heat Flux Distribution
The characteristics of film cooling in a CH4/O2 subscale chamber with multiinjector elements and two kinds of film cooling slot dimensions are investigated using a calorimeter chamber in experiments and simulations, in which the finite rate chemistry with a reduced CH4/O2 reaction mechanism is taken into account. The computed wall heat flux and pressure distributions are compared to the experimental results, which overall show good agreement. A large slot dimension is shown to induce mixing with core flow. This mixing causes a low heat-flux distribution near face plate along with high combustion efficiency.
8
Development Testing of a LOX/Methane Engine for In-Space Propulsion
D. C. Judd, S. Buccella, M. Alkema et al. · 2006 · 27 citations
Engineering, Aerospace Engineering, Mechanical Engineering +17
Numerical Study of Heat Transfer in Film Cooled Thrust Chambers
Barbara Betti, Emanuele Martelli, Francesco Nasuti et al. · 2012 · 17 citations
Engineering, Aerospace Engineering, Mechanical Engineering +17