Optimization of Non-Axisymmetric End-Wall Profiling in a High Pressure Turbine Stator Row

　　The influence of the squealer rim thickness on the tip leakage flow and heat transfer characteristics of the gas turbine blade was numerical investigated us

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Gas Turbine BladeSquealer TipLeakage FlowHeat Transfer

A New Thought on the Double-Solution Problem of the Mach Number at the Mixer Outlet of the Supersoni

　　During the take-off course of the Rocket-Based Combined Cycle ( RBCC ) engine,the embedded strut-jet rocket in itself is a supersonic ejector.In the quasi-1

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RBCCSupersonic ejectorQuasi-1D theoryDouble-solution problemunstable subsoni

Stereoscopic PIV Measurement of the Jet in Supersonic Crossflow and Spatial Correlation of Velocity

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Stereoscopic PIVJet in Supersonic CrossflowVelocity FluctuationSpatial Correl

Investigation of boundary layer development in Low Pressure Turbine Cascades with unsteady incoming

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PropulsionGas turbine engineLow Pressure TurbineProfile lossBoundary Layer

Three-Dimensional Shock WaveBoundary LayerCombustion Interactions in a Dual-Mode Scramjet Combustor

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Dual Mode ScramjetSupersonic CombustionShock Train -Combustion InteractionSho

Magnetohydrodynamic Energy Conversion with Supersonic Argon Plasma Flow

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MagnetohydrodynamicsElectrical Power GenerationSupersonic Plasma Flow

Optimization of Non-Axisymmetric End-Wall Profiling in a High Pressure Turbine Stator Row

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