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, und David E. Ashpis,

Veröffentlicht/Copyright: 1. Dezember 2000

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Aus der Zeitschrift International Journal of Turbo and Jet Engines Band 17 Heft 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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Published Online: 2000-12

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Artikel in diesem Heft

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?

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

Artikel in diesem Heft

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?