Performance Evaluation of a Two-stage Axial-flow Turbine for Two Values of Tip Clearance PDF Download
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Author: Milton G. Kofskey
Publisher:
ISBN:
Category : Axial flow
Languages : en
Pages : 28
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Book Description
Author: Milton G. Kofskey
Publisher:
ISBN:
Category : Axial flow
Languages : en
Pages : 28
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Book Description
Author: Milton G. Kofskey
Publisher:
ISBN:
Category : Axial flow
Languages : en
Pages : 0
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Book Description
Author: Milton G. Kofskey
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
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Book Description
Author: Milton G. Kofskey
Publisher:
ISBN:
Category : Liquid propellant rocket engines
Languages : en
Pages : 42
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Book Description
Author: Milton G. Kofskey
Publisher:
ISBN:
Category : Axial flow
Languages : en
Pages : 36
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
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Book Description
Author: Donald E. Holeski
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ISBN:
Category :
Languages : en
Pages : 4
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
The method of turbine performance prediction developed by Vavra and Eckert has been refined in this analysis to realize more of the potential of the three-dimensional calculating methods. Mach number and rotor tip clearance effects on blade outlet angles and loss coefficients have been localized rather than averaged over the blade height. An approximation for streamline curvature has been used. Performance curves were determined for two single stage axial-flow turbines. Test results were available for one of the turbines. Agreement between predicted and experimental performance values was generally within 3 per cent. (Author).
Author:
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ISBN:
Category :
Languages : en
Pages : 614
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Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1716
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Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index
