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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概要
- 論文の詳細を見る
- 一般社団法人日本機械学会の論文
- 1987-11-16
著者
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INOUE Masahiro
Kyushu Univ
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Fukuhara Minoru
Kyushu University
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KUROUMARU Motoo
Mitsubishi Heavy Industries, Ltd.
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FUKUHARA Minoru
Mitsubishi Heavy Industries, Ltd.
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EGUCHI Tsuyoshi
Mitsubishi Heavy Industries, Ltd.
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KUROUMARU Motoo
Kyushu University
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Inoue Masahiro
Kyushu University
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Eguchi Tsuyoshi
Mitsubishi Heavy Industries Ltd.
関連論文
- 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)