A standard k-epsilon RANS simulation of the Allison T56 combustor gives peak temperatures near 2306 K and wall stresses that follow the temperature field, but the claimed test-bench validation is not shown.
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Simulation and analysis of turbulent flame and its effect on the wall of aero engine combustor
A standard k-epsilon RANS simulation of the Allison T56 combustor gives peak temperatures near 2306 K and wall stresses that follow the temperature field, but the claimed test-bench validation is not shown.