Publication | Closed Access
The effect of mismatching between combustor and HP vanes on the aerodynamics and heat load in a 1-1/2 stages turbine
28
Citations
47
References
2019
Year
EngineeringAerospace EngineeringSupersonic CombustionCombustion ScienceGas Turbine CombustionHeat LoadIn-cylinder FlowAerodynamicsHp VanesTurbulent FlameHeat TransferGas Turbine Engine1-1/2 Stages
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