INOUE Masahiro | Kyushu Univ

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著作論文

Temperature Distributions in the Transonic Duct with Swept-back Bump by Laser-induced Fluorescence Method
Compatibility of Transonic Flows at Thick Trailing Edge in Turbine Blade Row
Unsteady Flow Behavior Due to Breakdown of Tip Leakage Vortex Visualized by Identifying the Vortex Cores
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
Effect of Tip Clearance on Casing Boundary Layer in an Isolated Axial Compressor Rotor : Series B : Fluids Engineering, Heat Transfer, Combustion, Power, Thermophysical Properties
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,
Development of End-Bent/Swept Blade for Multistage Axial Compressors(Dissertation Prize,GTSJ Prize)
Development of End-Bent/Swept Blade for Multistage Axial Compressors
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
ORGANIZED SESSION I: ROTATING STALL AND SURGE IN COMPRESSORS(Reports on Organized Sessions,1991 Yokohama International Gas Turbine Congress)

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