The prediction of transient phenomena inside liquid rocket engines has not been feasible until now because of the many challenges posed by the operating conditions. Especially, the departure from ideal gas (because of cryogenic injection) is one of the major hurdle for such simulations. In order to begin addressing these issue, a real-gas model has been implemented in a massively parallel flow solver. This solver is capable of performing Large-Eddy Simulations in geometrical configurations ranging from an axisymmetric slice to a 3D slice up to a full 3D combustor. Results show the importance of the unsteady dynamics of the flow,.
download Real Gas Simulations of a Sub-Scale Liquid Rocket Engine: Unsteady Simulations and Transient Heat Transfer in a Real Gas Environment pdf free
Real Gas Simulations of a Sub-Scale Liquid Rocket Engine: Unsteady Simulations and Transient Heat Transfer in a Real Gas Environment read online free book
Real Gas Simulations of a Sub-Scale Liquid Rocket Engine: Unsteady Simulations and Transient Heat Transfer in a Real Gas Environment books pdf online
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