Effect of Tip Clearance on Casing Boundary Layer in an Isolated Axial Compressor Rotor : Series B : Fluids Engineering, Heat Transfer, Combustion, Power, Thermophysical Properties

スポンサーリンク

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
• 1987-08-15

著者

• INOUE Masahiro

  Kyushu Univ

• Fukuhara Minoru

  Kyushu University

• KUROUMARU Motoo

  Kyushu University

• BEKKI Toshihiko

  Kyushu University

• Inoue Masahiro

  Kyushu University

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)

スポンサーリンク