Inoue Masahiro | Kyushu University

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著作論文

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,
ORGANIZED SESSION I: ROTATING STALL AND SURGE IN COMPRESSORS(Reports on Organized Sessions,1991 Yokohama International Gas Turbine Congress)

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