Air-performance Evaluation of a 4.0-inch-mean-diameter Single-stage Turbine at Various Inlet Pressures from 0.14 to 1.88 Atmospheres and Corresponding Reynolds Numbers from 2500 to 50,000 PDF Download
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Author: Robert Y. Wong
Publisher:
ISBN:
Category : Air pressure
Languages : en
Pages : 44
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Book Description
Author: Robert Y. Wong
Publisher:
ISBN:
Category : Air pressure
Languages : en
Pages : 44
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Book Description
Author: Robert Y. Wong
Publisher:
ISBN:
Category :
Languages : en
Pages : 39
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Book Description
Author: Hugh A. Klassen
Publisher:
ISBN:
Category : Axial flow
Languages : en
Pages : 34
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Book Description
Author: Ernest R. Chanes
Publisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 34
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Book Description
Efficiency tests have been conducted on a single-stage impulse turbine having a 13.2-inch pitch-line diameter wheel and a cast nozzle diaphragm over a range of turbine speeds from 3000 to 17,000 rpm pressure ratios from 1.5 to 5.0, inlet total temperatures from 1200 to 2000 degrees R, and inlet total pressures from 18 to 59 inches of mercury absolute. The effect of inlet temperature and pressure on turbine efficiency for constant pressure ratio and blade-to-jet speed ratio is correlated against a factor derived from the equation for Reynolds number. The degree of correlation indicates that the change in turbine efficiency with inlet temperature and pressure for constant pressure ratio and blade-to-jet speed ratio is principally a Reynolds number test.
Author: Hugh A. Klassen
Publisher:
ISBN:
Category : Axial flow
Languages : en
Pages : 23
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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: Hugh A. Klassen
Publisher:
ISBN:
Category :
Languages : en
Pages : 23
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Book Description
Author: John C. Freche
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 22
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Book Description
Author: William J. Nusbaum
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
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Book Description
Author: Meherwan P. Boyce
Publisher: Elsevier
ISBN: 0080456898
Category : Mathematics
Languages : en
Pages : 956
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Book Description
The Gas Turbine Engineering Handbook has been the standard for engineers involved in the design, selection, and operation of gas turbines. This revision includes new case histories, the latest techniques, and new designs to comply with recently passed legislation. By keeping the book up to date with new, emerging topics, Boyce ensures that this book will remain the standard and most widely used book in this field. The new Third Edition of the Gas Turbine Engineering Hand Book updates the book to cover the new generation of Advanced gas Turbines. It examines the benefit and some of the major problems that have been encountered by these new turbines. The book keeps abreast of the environmental changes and the industries answer to these new regulations. A new chapter on case histories has been added to enable the engineer in the field to keep abreast of problems that are being encountered and the solutions that have resulted in solving them. Comprehensive treatment of Gas Turbines from Design to Operation and Maintenance. In depth treatment of Compressors with emphasis on surge, rotating stall, and choke; Combustors with emphasis on Dry Low NOx Combustors; and Turbines with emphasis on Metallurgy and new cooling schemes. An excellent introductory book for the student and field engineers A special maintenance section dealing with the advanced gas turbines, and special diagnostic charts have been provided that will enable the reader to troubleshoot problems he encounters in the field The third edition consists of many Case Histories of Gas Turbine problems. This should enable the field engineer to avoid some of these same generic problems
