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 PDF Author: Anthony J. Diaguila
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ISBN:
Category : Aeronautics
Languages : en
Pages : 28

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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 PDF Author: Anthony J. Diaguila
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 28

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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 258

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National Bureau of Standards Circular

National Bureau of Standards Circular PDF Author:
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ISBN:
Category :
Languages : en
Pages : 122

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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 PDF Author: John C. Freche
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ISBN:
Category : Aeronautics
Languages : en
Pages : 30

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Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category :
Languages : en
Pages : 596

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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 PDF Author: Arthur N. Curren
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ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 42

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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 PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568

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Circular of the Bureau of Standards

Circular of the Bureau of Standards PDF Author:
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Category : Weights and measures
Languages : en
Pages : 122

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
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Category : Aeronautics
Languages : en
Pages : 750

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Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages :

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.