ORGANIZED SESSION I: ROTATING STALL AND SURGE IN COMPRESSORS(Reports on Organized Sessions,1991 Yokohama International Gas Turbine Congress)
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概要
著者
関連論文
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Temperature Distributions in the Transonic Duct with Swept-back Bump by Laser-induced Fluorescence Method
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Compatibility of Transonic Flows at Thick Trailing Edge in Turbine Blade Row
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Unsteady Flow Behavior Due to Breakdown of Tip Leakage Vortex Visualized by Identifying the Vortex Cores
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Effect of Tip Clearance on Casing Boundary Layer in an Isolated Axial Compressor Rotor : 2nd Report, Variation with Inlet Boundary Layer Thickness : Series B : Fluid Engineering, Heat Transfer, Combustion, Power, Thermophysical Properties
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Effect of Tip Clearance on Casing Boundary Layer in an Isolated Axial Compressor Rotor : Series B : Fluids Engineering, Heat Transfer, Combustion, Power, Thermophysical Properties
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Numerical Methods for the Compressible Navier-Stokes Equations Using an Explicit Time-Marching Technique (Comparison Between the Four Stage Runge-Kutta and Two Stage Rational Runge-Kutta Schemes) : Series B : Fluids Engineering, Heat Transfer, Combustion,
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Development of End-Bent/Swept Blade for Multistage Axial Compressors(Dissertation Prize,GTSJ Prize)
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Development of End-Bent/Swept Blade for Multistage Axial Compressors
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Studies on the Three-dimensional Flow Field in a Turbine Scroll (1st Report, Measurements of Secondary Flows) : Series B : Fluids Engineering, Heat Transfer, Combustion, Power, Thermophysical Properties
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ORGANIZED SESSION I: ROTATING STALL AND SURGE IN COMPRESSORS(Reports on Organized Sessions,1991 Yokohama International Gas Turbine Congress)
スポンサーリンク