Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material

Zhen-Xue Han,; Brian H. Dennis,; George S. Dulikravich,

doi:10.1515/TJJ.2001.18.1.47

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Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material

Zhen-Xue Han, , Brian H. Dennis, and George S. Dulikravich,

Published/Copyright: March 1, 2001

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From the journal International Journal of Turbo and Jet Engines Volume 18 Issue 1

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Harvard
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Vancouver

Han,, Zhen-Xue, Dennis,, Brian H. and Dulikravich,, George S.. "Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material" International Journal of Turbo and Jet Engines, vol. 18, no. 1, pp. 47-58. https://doi.org/10.1515/TJJ.2001.18.1.47

Han,, Z., Dennis,, B. & Dulikravich,, G. (). Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material. International Journal of Turbo and Jet Engines, 18(1), 47-58. https://doi.org/10.1515/TJJ.2001.18.1.47

Han,, Z., Dennis,, B. and Dulikravich,, G. () Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material. International Journal of Turbo and Jet Engines, Vol. 18 (Issue 1), pp. 47-58. https://doi.org/10.1515/TJJ.2001.18.1.47

Han,, Zhen-Xue, Dennis,, Brian H. and Dulikravich,, George S.. "Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material" International Journal of Turbo and Jet Engines 18, no. 1 (): 47-58. https://doi.org/10.1515/TJJ.2001.18.1.47

Han, Z, Dennis, B, Dulikravich, G. Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material. International Journal of Turbo and Jet Engines. ;18(1): 47-58. https://doi.org/10.1515/TJJ.2001.18.1.47

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CONTENTS
The Effects of Blade Count on Boundary Layer Development in a Low-Pressure Turbine
Effects of Hot Streak Shape on Rotor Heating in a High-Subsonic Single-Stage Turbine
A Simple Method for Geometry Definition of Radial Compressors
Advanced Aerothermodynamics Associated with Clean Technologies for Upgrading Gas Turbines in Simple and Combined-Cycle Power Stations
Thrust Vectoring Flight Control To Maximize Future Jet Transport Flight Safety
Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material
A Simple Mobile Anechoic Chamber For Experiments in Jet Acoustics
The Influence of Fuel Droplet Characteristics on Chemical Mechanisms in a Premixed Laminar Spray Flame

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https://doi.org/10.1515/TJJ.2001.18.1.47

Articles in the same Issue

CONTENTS
The Effects of Blade Count on Boundary Layer Development in a Low-Pressure Turbine
Effects of Hot Streak Shape on Rotor Heating in a High-Subsonic Single-Stage Turbine
A Simple Method for Geometry Definition of Radial Compressors
Advanced Aerothermodynamics Associated with Clean Technologies for Upgrading Gas Turbines in Simple and Combined-Cycle Power Stations
Thrust Vectoring Flight Control To Maximize Future Jet Transport Flight Safety
Simultaneous Prediction of External Flow-Field and Temperature in Internally Cooled 3-D Turbine Blade Material
A Simple Mobile Anechoic Chamber For Experiments in Jet Acoustics
The Influence of Fuel Droplet Characteristics on Chemical Mechanisms in a Premixed Laminar Spray Flame