Numerical Flow Analysis of Fully Three—Dimensional Turbine Cascades

Masahiko Koya,; Susumu Kotake,

doi:10.1515/TJJ.1985.2.1.45

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Numerical Flow Analysis of Fully Three—Dimensional Turbine Cascades

Masahiko Koya, and Susumu Kotake,

Published/Copyright: March 1, 1985

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From the journal International Journal of Turbo and Jet Engines Volume 2 Issue 1

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Koya,, Masahiko and Kotake,, Susumu. "Numerical Flow Analysis of Fully Three—Dimensional Turbine Cascades" International Journal of Turbo and Jet Engines, vol. 2, no. 1, pp. 45-56. https://doi.org/10.1515/TJJ.1985.2.1.45

Koya,, M. & Kotake,, S. (). Numerical Flow Analysis of Fully Three—Dimensional Turbine Cascades. International Journal of Turbo and Jet Engines, 2(1), 45-56. https://doi.org/10.1515/TJJ.1985.2.1.45

Koya,, M. and Kotake,, S. () Numerical Flow Analysis of Fully Three—Dimensional Turbine Cascades. International Journal of Turbo and Jet Engines, Vol. 2 (Issue 1), pp. 45-56. https://doi.org/10.1515/TJJ.1985.2.1.45

Koya,, Masahiko and Kotake,, Susumu. "Numerical Flow Analysis of Fully Three—Dimensional Turbine Cascades" International Journal of Turbo and Jet Engines 2, no. 1 (): 45-56. https://doi.org/10.1515/TJJ.1985.2.1.45

Koya, M, Kotake, S. Numerical Flow Analysis of Fully Three—Dimensional Turbine Cascades. International Journal of Turbo and Jet Engines. ;2(1): 45-56. https://doi.org/10.1515/TJJ.1985.2.1.45

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Published Online: 1985-03

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Articles in the same Issue

CONTENTS
Performance Comparison Between Transpiration Air Cooled Turbine 3000°F (1649°C) Stator Vanes and Solid Uncooled Vanes
Torsional/Lateral Coupling in Geared Rotors
Turbotrans — Α Programming Language for the Performance Simulation of Arbitrary Gas Turbine Engines with Arbitrary Control Systems
Turbotest - A Computer Program for Rig Test Analysis of Arbitrary Gas Turbine Engines
The Thermal Stability of Aviation Fuel
Numerical Flow Analysis of Fully Three—Dimensional Turbine Cascades
Gas Turbine for Pressurising a Fluidised Bed Combustion System
Double-Decked Gas Turbine with Compact Heat Eschanger
Cogeneration and Multiple Heat Recovery
Simulation of Surge Margin Changes Due to Heat Transfer Effects in Gas Turbine Transients

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https://doi.org/10.1515/TJJ.1985.2.1.45

Articles in the same Issue

CONTENTS
Performance Comparison Between Transpiration Air Cooled Turbine 3000°F (1649°C) Stator Vanes and Solid Uncooled Vanes
Torsional/Lateral Coupling in Geared Rotors
Turbotrans — Α Programming Language for the Performance Simulation of Arbitrary Gas Turbine Engines with Arbitrary Control Systems
Turbotest - A Computer Program for Rig Test Analysis of Arbitrary Gas Turbine Engines
The Thermal Stability of Aviation Fuel
Numerical Flow Analysis of Fully Three—Dimensional Turbine Cascades
Gas Turbine for Pressurising a Fluidised Bed Combustion System
Double-Decked Gas Turbine with Compact Heat Eschanger
Cogeneration and Multiple Heat Recovery
Simulation of Surge Margin Changes Due to Heat Transfer Effects in Gas Turbine Transients