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- W2331926342 abstract "Inter-turbine burners are useful devices for increasing engine power. To enable inter-turbine burners for aviation applications the size of combustion devices needs to be reduced. High-g ultra-compact combustors (UCC) are a technology for reducing the size of combustors. In these combustors the fuel and air are swirled around the centerline at velocities large enough to impact centrifugal forces. In this work, the large eddy simulation (LES) method is used to understand mixing and flow dynamics inside centrifugal-based combustion systems. Simulation results show that mixing of fuel and oxidizer is based on a jet-in-crossflow system, with the fuel jet issuing into a circulating oxidizer flow stream. The momentum ratio between the jet and the crossflow determine fuel penetration, and will determine combustion eciency. Simulation results exhibit significant entrainment of fuel into recirculation zones inside the combustor, however more extensive experimental data is required to validate this result. ⇢ Filtered density ej Filtered velocity f ˙ W Filtered evaporation source term ˜ P Filtered pressure ⌧ij Viscous stress tensor Tij Sub filter stresses F Drag force" @default.
- W2331926342 created "2016-06-24" @default.
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- W2331926342 date "2013-01-05" @default.
- W2331926342 modified "2023-09-27" @default.
- W2331926342 title "Large Eddy Simulation Analysis of Flow Field Inside a High-g Combustor" @default.
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- W2331926342 doi "https://doi.org/10.2514/6.2013-1140" @default.
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