Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows

Daniel J. Dorney,; James P. Lake,; Paul I. King,; David E. Ashpis,

doi:10.1515/TJJ.2000.17.4.241

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Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows

Daniel J. Dorney, , James P. Lake, , Paul I. King, and David E. Ashpis,

Published/Copyright: December 1, 2000

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From the journal International Journal of Turbo and Jet Engines Volume 17 Issue 4

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Dorney,, Daniel J., Lake,, James P., King,, Paul I. and Ashpis,, David E.. "Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows" International Journal of Turbo and Jet Engines, vol. 17, no. 4, 2000, pp. 241-254. https://doi.org/10.1515/TJJ.2000.17.4.241

Dorney,, D., Lake,, J., King,, P. & Ashpis,, D. (2000). Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows. International Journal of Turbo and Jet Engines, 17(4), 241-254. https://doi.org/10.1515/TJJ.2000.17.4.241

Dorney,, D., Lake,, J., King,, P. and Ashpis,, D. (2000) Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows. International Journal of Turbo and Jet Engines, Vol. 17 (Issue 4), pp. 241-254. https://doi.org/10.1515/TJJ.2000.17.4.241

Dorney,, Daniel J., Lake,, James P., King,, Paul I. and Ashpis,, David E.. "Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows" International Journal of Turbo and Jet Engines 17, no. 4 (2000): 241-254. https://doi.org/10.1515/TJJ.2000.17.4.241

Dorney, D, Lake, J, King, P, Ashpis, D. Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows. International Journal of Turbo and Jet Engines. 2000;17(4): 241-254. https://doi.org/10.1515/TJJ.2000.17.4.241

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CONTENTS
Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows
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Maximizing Multistage Turbine Efficiency by Optimizing Hub and Shroud Shapes and Inlet and Exit Conditions of Each Blade Row
Experimental Evaluation of Precursors to Centrifugal Compressor Instability
3-D Inlet Guide Vane Generated Vortical Forcing Functions
Effect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip Clearance
A New Era of Jet Transport Safety By Advanced Legislation?

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https://doi.org/10.1515/TJJ.2000.17.4.241

Articles in the same Issue

CONTENTS
Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows
Characteristics of Arrays of Spray Diffusion Flames
Maximizing Multistage Turbine Efficiency by Optimizing Hub and Shroud Shapes and Inlet and Exit Conditions of Each Blade Row
Experimental Evaluation of Precursors to Centrifugal Compressor Instability
3-D Inlet Guide Vane Generated Vortical Forcing Functions
Effect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip Clearance
A New Era of Jet Transport Safety By Advanced Legislation?