Effects of Hot Streak/Airfoil Ratio in a High Subsonic Single-Stage Turbine

Daniel J. Dorney,; Douglas L. Sondak,; Paul G. Cizmas,

doi:10.1515/TJJ.2000.17.2.119

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Effects of Hot Streak/Airfoil Ratio in a High Subsonic Single-Stage Turbine

Daniel J. Dorney, , Douglas L. Sondak, and Paul G. Cizmas,

Published/Copyright: June 1, 2000

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From the journal International Journal of Turbo and Jet Engines Volume 17 Issue 2

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Vancouver

Dorney,, Daniel J., Sondak,, Douglas L. and Cizmas,, Paul G.. "Effects of Hot Streak/Airfoil Ratio in a High Subsonic Single-Stage Turbine" International Journal of Turbo and Jet Engines, vol. 17, no. 2, pp. 119-132. https://doi.org/10.1515/TJJ.2000.17.2.119

Dorney,, D., Sondak,, D. & Cizmas,, P. (). Effects of Hot Streak/Airfoil Ratio in a High Subsonic Single-Stage Turbine. International Journal of Turbo and Jet Engines, 17(2), 119-132. https://doi.org/10.1515/TJJ.2000.17.2.119

Dorney,, D., Sondak,, D. and Cizmas,, P. () Effects of Hot Streak/Airfoil Ratio in a High Subsonic Single-Stage Turbine. International Journal of Turbo and Jet Engines, Vol. 17 (Issue 2), pp. 119-132. https://doi.org/10.1515/TJJ.2000.17.2.119

Dorney,, Daniel J., Sondak,, Douglas L. and Cizmas,, Paul G.. "Effects of Hot Streak/Airfoil Ratio in a High Subsonic Single-Stage Turbine" International Journal of Turbo and Jet Engines 17, no. 2 (): 119-132. https://doi.org/10.1515/TJJ.2000.17.2.119

Dorney, D, Sondak, D, Cizmas, P. Effects of Hot Streak/Airfoil Ratio in a High Subsonic Single-Stage Turbine. International Journal of Turbo and Jet Engines. ;17(2): 119-132. https://doi.org/10.1515/TJJ.2000.17.2.119

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Published Online: 2000-06

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Articles in the same Issue

CONTENTS
Full-Annulus Simulations of Airfoil Clocking in A Compressor At Off-Design Operating Conditions
Effects of Hot Streak/Airfoil Ratio in a High Subsonic Single-Stage Turbine
The Influence of Clocking on Unsteady Forces of Compressor and Turbine Blades
A Variational Model for Compressible Rotational Blade-to-Blade Flow Using Liu-Type Potential Function
Experimental and Theoretical Frequency Response of Pressure Transducers For High Speed Turbomachinery
Comparison of Streamline Throughflow and Streamline Curvature Methods
Evaporation and Coalescence of Spray Droplets Comprised of Two-Component Fuels

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https://doi.org/10.1515/TJJ.2000.17.2.119

Articles in the same Issue

CONTENTS
Full-Annulus Simulations of Airfoil Clocking in A Compressor At Off-Design Operating Conditions
Effects of Hot Streak/Airfoil Ratio in a High Subsonic Single-Stage Turbine
The Influence of Clocking on Unsteady Forces of Compressor and Turbine Blades
A Variational Model for Compressible Rotational Blade-to-Blade Flow Using Liu-Type Potential Function
Experimental and Theoretical Frequency Response of Pressure Transducers For High Speed Turbomachinery
Comparison of Streamline Throughflow and Streamline Curvature Methods
Evaporation and Coalescence of Spray Droplets Comprised of Two-Component Fuels