Rotating Stall Performance and Recoverability of a High-speed 10-stage Axial-flow Compressor

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Rotating Stall Performance and Recoverability of a High-speed 10-stage Axial-flow Compressor by : W. W. Copenhaver

Download or read book Rotating Stall Performance and Recoverability of a High-speed 10-stage Axial-flow Compressor written by W. W. Copenhaver and published by . This book was released on 1989 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Stage Effects on Stalling and Recovery of a High-Speed 10-Stage Axial-Flow Compressor

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ISBN 13 :
Total Pages : 401 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Stage Effects on Stalling and Recovery of a High-Speed 10-Stage Axial-Flow Compressor by : William W. Copenhaver

Download or read book Stage Effects on Stalling and Recovery of a High-Speed 10-Stage Axial-Flow Compressor written by William W. Copenhaver and published by . This book was released on 1990 with total page 401 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results of a High-speed 10-stage axial-flow compressor test involving overall compressor and individual stage performance while stalling and operating in quasi-steady rotating stall are described. Test procedures and data acquisition methods used to obtain the dynamic stalling and quasi-steady in-stall data are explained. Unstalled and in-stall data obtained from the compressor operating at five different shaft speeds and one off-schedule variable vane condition are presented. The effects of compressor speed and variable geometry on overall compressor in-stall pressure rise and hysteresis extent are illustrated through the use of quasi-steady stage temperature and pressure rise characteristics. The results indicate that individual stage performance during overall compressor. Time resolved install data acquired at two different shaft speeds are presented in support of the notion that stage operation varies significantly from entrance to exit of the compressor. Both time-averaged and time-resolved individual stage results suggest that stage matching is important, not only for unstalled performance but also for in-stall performance and recoverability from stall. The measured high-speed 10-stage test compressor individual stage pressure and temperature characteristics were input into a stage-by-stage dynamic compressor performance model. The analytical model had been previously validated for the prediction of low-speed compressor stalling and in-stall performance. (SDW).

Stage Effects on Stalling and Recovery of a High-speed 10-stage Axial- Flow Compressor

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ISBN 13 :
Total Pages : 748 pages
Book Rating : 4.:/5 (23 download)

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Book Synopsis Stage Effects on Stalling and Recovery of a High-speed 10-stage Axial- Flow Compressor by : William Ward Copenhaver

Download or read book Stage Effects on Stalling and Recovery of a High-speed 10-stage Axial- Flow Compressor written by William Ward Copenhaver and published by . This book was released on 1988 with total page 748 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 772 pages
Book Rating : 4.:/5 (31 download)

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Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 772 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Compressor Surge and Stall

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ISBN 13 :
Total Pages : 532 pages
Book Rating : 4.X/5 (4 download)

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Book Synopsis Compressor Surge and Stall by : R. C. Pampreen

Download or read book Compressor Surge and Stall written by R. C. Pampreen and published by . This book was released on 1993 with total page 532 pages. Available in PDF, EPUB and Kindle. Book excerpt: High efficiency axial and centrifugal compressors are important in fields as diverse as aircraft engines, superchargers and turbochargers, process and refrigeration compressors. Compressors must achieve high efficiency in blade rows in diffusing flow fields. Of equal and sometimes greater importance is the range os stable operation of the compressor. Blade row stall characteristics determine the limit os stable operation. Blading can stall uniformly with symmetric flow breakdown or asymmetrically in rotating stall, wich propagates around the periphery of the blade row. Depending on aerodynamic conditions, surge may occur instead of, in concert with, or subsequent to blade row stall. The transient breakdown and recovery of aerodynamic loading not only limits compressor performance but also leads to mechanical failures caused by the vibrational loads imposed on the blades. There is no need to know what initiates these performance limits so that surge and stall margins can be optimized and control strategies can be planned. the first step toward understanding is to be knowledgeable about he physical processes occurring during surge and stall. This will permit the designer to anticipate variable geometry needs such as variable inlet guide vanes, variable statuors, and bleed port strategies. Theoritical treatment is far from being well established, however, there are many approaches discussed in the literature. This book is a unique reference to the subject matter. Physical descriptions of the phenomena are given, test results are presented, and analytical studies are discussed. There has been much written about the experimental investigations and theoretical treatments related to surge and stall. To assist those who would pursue advancements in furthering ou knowledge of surge and stall, it seemed appropriate to have a resource that contains a compendium of information on this subject. That is the purpose of this book. [Source : d'après la 4e de couverture].

Rotating Stall Investigation of the 0.72 Hub-tip Ratio Single-stage Compressor

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ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Rotating Stall Investigation of the 0.72 Hub-tip Ratio Single-stage Compressor by : Robert W. Graham

Download or read book Rotating Stall Investigation of the 0.72 Hub-tip Ratio Single-stage Compressor written by Robert W. Graham and published by . This book was released on 1954 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Papers Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference

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ISBN 13 :
Total Pages : 488 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis Papers Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference by :

Download or read book Papers Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference written by and published by . This book was released on 1989 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Applied Mechanics Reviews

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ISBN 13 :
Total Pages : 606 pages
Book Rating : 4.F/5 ( download)

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Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1954 with total page 606 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Design of Axial-flow Compressors

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ISBN 13 :
Total Pages : 542 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Aerodynamic Design of Axial-flow Compressors by : Lewis Research Center

Download or read book Aerodynamic Design of Axial-flow Compressors written by Lewis Research Center and published by . This book was released on 1965 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Design of Axial Flow Compressors

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ISBN 13 :
Total Pages : 552 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic Design of Axial Flow Compressors by : Robert O. Bullock

Download or read book Aerodynamic Design of Axial Flow Compressors written by Robert O. Bullock and published by . This book was released on 1965 with total page 552 pages. Available in PDF, EPUB and Kindle. Book excerpt:

International Aerospace Abstracts

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ISBN 13 :
Total Pages : 514 pages
Book Rating : 4.3/5 (91 download)

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Download or read book International Aerospace Abstracts written by and published by . This book was released on 1997 with total page 514 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Analysis of Rotating Stall Onset in High-speed Axial Flow Compressors

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Analysis of Rotating Stall Onset in High-speed Axial Flow Compressors by : G. J. Hendricks

Download or read book Analysis of Rotating Stall Onset in High-speed Axial Flow Compressors written by G. J. Hendricks and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA SP.

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ISBN 13 :
Total Pages : 590 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA SP. by :

Download or read book NASA SP. written by and published by . This book was released on 1993 with total page 590 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Engineering Fluid Dynamics 2018

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Publisher : MDPI
ISBN 13 : 3039281127
Total Pages : 256 pages
Book Rating : 4.0/5 (392 download)

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Book Synopsis Engineering Fluid Dynamics 2018 by : Bjørn H. Hjertager

Download or read book Engineering Fluid Dynamics 2018 written by Bjørn H. Hjertager and published by MDPI. This book was released on 2020-01-15 with total page 256 pages. Available in PDF, EPUB and Kindle. Book excerpt: “Engineering Fluid Dynamics 2018”. The topic of engineering fluid dynamics includes both experimental as well as computational studies. Of special interest were submissions from the fields of mechanical, chemical, marine, safety, and energy engineering. We welcomed both original research articles as well as review articles. After one year, 28 papers were submitted and 14 were accepted for publication. The average processing time was 37.91 days. The authors had the following geographical distribution: China (9); Korea (3); Spain (1); and India (1). Papers covered a wide range of topics, including analysis of fans, turbines, fires in tunnels, vortex generators, deep sea mining, as well as pumps.

NASA Scientific and Technical Publications

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ISBN 13 :
Total Pages : 410 pages
Book Rating : 4.F/5 ( download)

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Download or read book NASA Scientific and Technical Publications written by and published by . This book was released on 1987 with total page 410 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Over-all Performance, Rotating Stall, and Blade Vibration at Low and Intermediate Compressor Speeds

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ISBN 13 :
Total Pages : 21 pages
Book Rating : 4.:/5 (254 download)

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Book Synopsis Over-all Performance, Rotating Stall, and Blade Vibration at Low and Intermediate Compressor Speeds by : Raymond M. Standahar

Download or read book Over-all Performance, Rotating Stall, and Blade Vibration at Low and Intermediate Compressor Speeds written by Raymond M. Standahar and published by . This book was released on 1955 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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ISBN 13 :
Total Pages : 450 pages
Book Rating : 4.X/5 (4 download)

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Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :

Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1960 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt: