Blade-to-coolant Heat-transfer Results and Operating Data from a Natural-convection Water-cooled Single-stage Turbine

Blade-to-coolant Heat-transfer Results and Operating Data from a Natural-convection Water-cooled Single-stage Turbine
Title Blade-to-coolant Heat-transfer Results and Operating Data from a Natural-convection Water-cooled Single-stage Turbine PDF eBook
Author Anthony J. Diaguila
Publisher
Pages 28
Release 1951
Genre Aeronautics
ISBN

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Determination of Blade-to-coolant Heat-transfer Coefficients on a Forced-convection, Water-cooled, Single-stage Turbine

Determination of Blade-to-coolant Heat-transfer Coefficients on a Forced-convection, Water-cooled, Single-stage Turbine
Title Determination of Blade-to-coolant Heat-transfer Coefficients on a Forced-convection, Water-cooled, Single-stage Turbine PDF eBook
Author John C. Freche
Publisher
Pages 30
Release 1951
Genre Aeronautics
ISBN

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Index of NACA Technical Publications

Index of NACA Technical Publications
Title Index of NACA Technical Publications PDF eBook
Author United States. National Advisory Committee for Aeronautics
Publisher
Pages 258
Release 1953
Genre Aeronautics
ISBN

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National Bureau of Standards Circular

National Bureau of Standards Circular
Title National Bureau of Standards Circular PDF eBook
Author
Publisher
Pages 122
Release 1954
Genre
ISBN

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Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice
Title Research Abstracts and Reclassification Notice PDF eBook
Author United States. National Advisory Committee for Aeronautics
Publisher
Pages 596
Release 1951
Genre
ISBN

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Effect of Diameter of Closed-end Coolant Passages on Natural-convection Water Cooling of Gas-turbine Blades

Effect of Diameter of Closed-end Coolant Passages on Natural-convection Water Cooling of Gas-turbine Blades
Title Effect of Diameter of Closed-end Coolant Passages on Natural-convection Water Cooling of Gas-turbine Blades PDF eBook
Author Arthur N. Curren
Publisher
Pages 42
Release 1956
Genre Charts, diagrams, etc
ISBN

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An experimental investigation on a water-cooled gas turbine with blade coolant-passage diameters ranging from 0.100 to 0.500 inch, corresponding to length-to-diameter ratios of 25.5 to 5.1, in various quadrants of the turbine. The investigation was conducted to determine (1) whether coolant-passage length-to-ratio has a significant effect on natural-convection heat-transfer correlation, and (2) whether turbine blade temperatures could be calculated with reasonable accuracy from a theoretical natural-convection heat-transfer correlation.

Research Abstracts

Research Abstracts
Title Research Abstracts PDF eBook
Author United States. National Advisory Committee for Aeronautics
Publisher
Pages 568
Release 1951
Genre Aeronautics
ISBN

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