The Effects of Blade Count on Boundary Layer Development in a Low-Pressure Turbine

Daniel J. Dorney,; Horia C. Flitan,; David E. Ashpis,; William J. Solomon,

doi:10.1515/TJJ.2001.18.1.1

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The Effects of Blade Count on Boundary Layer Development in a Low-Pressure Turbine

Daniel J. Dorney, , Horia C. Flitan, , David E. Ashpis, and William J. Solomon,

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
Chicago
Vancouver

Dorney,, Daniel J., Flitan,, Horia C., Ashpis,, David E. and Solomon,, William J.. "The Effects of Blade Count on Boundary Layer Development in a Low-Pressure Turbine" International Journal of Turbo and Jet Engines, vol. 18, no. 1, 2001, pp. 1-14. https://doi.org/10.1515/TJJ.2001.18.1.1

Dorney,, D., Flitan,, H., Ashpis,, D. & Solomon,, W. (2001). The Effects of Blade Count on Boundary Layer Development in a Low-Pressure Turbine. International Journal of Turbo and Jet Engines, 18(1), 1-14. https://doi.org/10.1515/TJJ.2001.18.1.1

Dorney,, D., Flitan,, H., Ashpis,, D. and Solomon,, W. (2001) The Effects of Blade Count on Boundary Layer Development in a Low-Pressure Turbine. International Journal of Turbo and Jet Engines, Vol. 18 (Issue 1), pp. 1-14. https://doi.org/10.1515/TJJ.2001.18.1.1

Dorney,, Daniel J., Flitan,, Horia C., Ashpis,, David E. and Solomon,, William J.. "The Effects of Blade Count on Boundary Layer Development in a Low-Pressure Turbine" International Journal of Turbo and Jet Engines 18, no. 1 (2001): 1-14. https://doi.org/10.1515/TJJ.2001.18.1.1

Dorney, D, Flitan, H, Ashpis, D, Solomon, W. The Effects of Blade Count on Boundary Layer Development in a Low-Pressure Turbine. International Journal of Turbo and Jet Engines. 2001;18(1): 1-14. https://doi.org/10.1515/TJJ.2001.18.1.1

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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

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https://doi.org/10.1515/TJJ.2001.18.1.1

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