Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Download Investigation Of Axial Flow Compressor Surge full books in PDF, epub, and Kindle. Read online Investigation Of Axial Flow Compressor Surge ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author : Walter D. Hoffmann
Publisher :
ISBN 13 :
Total Pages : 134 pages
Book Rating : 4.:/5 (381 download)
Download or read book Investigation of Axial-flow Compressor Surge written by Walter D. Hoffmann and published by . This book was released on 1955 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Patrick M. Russler
Publisher :
ISBN 13 :
Total Pages : 330 pages
Book Rating : 4.:/5 (281 download)
Download or read book An Investigation of the Surge Behavior of a High-speed Ten-stage Axial Flow Compressor written by Patrick M. Russler and published by . This book was released on 1993 with total page 330 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Patrick M. Russler
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (281 download)
Download or read book An Investigation of the Surge Behavior of a High-speed Ten-stage Axial Flow Compressor written by Patrick M. Russler and published by . This book was released on 1993 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Ross D. Schmidt
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.3/5 (91 download)
Download or read book Determination of Surge and Stall Limits of an Axial-flow Turbojet Engine for Control Applications written by Ross D. Schmidt and published by . This book was released on 1953 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: During the course of an investigation of an axial-flow turbojet engine in the Lewis altitude wind tunnel, limitations on the transient operation of the engine were determined to relation to two altitudes and exhaust-nozzle-areas. Below approximately 70 percent of the generalized engine rotational speed, a high-frequency oscillation (stall) at the compressor inlet limited transient operation of the engine. Over 70 percent of the engine speed, transient operation was limited by a low-frequency oscillation (surge), which occurred throughout the engine.
Author : Lewis Research Center
Publisher :
ISBN 13 :
Total Pages : 542 pages
Book Rating : 4.F/5 ( download)
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:
Author : Ronald H. Aungier
Publisher : American Society of Mechanical Engineers
ISBN 13 :
Total Pages : 386 pages
Book Rating : 4.3/5 (91 download)
Download or read book Axial-flow Compressors written by Ronald H. Aungier and published by American Society of Mechanical Engineers. This book was released on 2003 with total page 386 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book provides a thorough description of an aerodynamic design and analysis systems for Axial-Flow Compressors. It describes the basic fluid dynamic and thermodynamic principles, empirical models and numerical methods used for the full range of procedures and analytical tools that an engineer needs for virtually any tupe of Axial-Flow Compressor, aerodynamic design or analysis activity. It reviews and evaluates several design strategies that have been recommended in the literature or which have been found to be effective. It gives a complete description of an actual working system, such that readers can implement all or part of the system. Engineers responsible for developing, maintaining of improving design and analysis systems can benefit greatly from this type of reference. The technology has become so complex and the role of computers so pervasive that about the only way this can be done today is to concentrate on a specific design and analysis system. The author provides practical methodology as well as the details needed to implement the suggested procedures.
Author : Ray E. Budinger
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.3/5 (91 download)
Download or read book Investigation of the Performance of a Turbojet Engine with Variable-position Compressor Inlet Guide Vanes written by Ray E. Budinger and published by . This book was released on 1955 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : R. C. Pampreen
Publisher :
ISBN 13 :
Total Pages : 532 pages
Book Rating : 4.X/5 (4 download)
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].
Author :
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (317 download)
Download or read book An Investigation of Surge in a High-Speed Centrifugal Compressor Using Digital PIV written by and published by . This book was released on 2002 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Royce Nolan Brown
Publisher :
ISBN 13 :
Total Pages : 206 pages
Book Rating : 4.:/5 (89 download)
Download or read book An Experimental Investigation of a Pneumatic Closed Loop Anti-surge Control for Centrifugal and Axial Flow Compressors written by Royce Nolan Brown and published by . This book was released on 1966 with total page 206 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Merle C. Huppert
Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (11 download)
Download or read book Preliminary Investigation of Flow Fluctuations During Surge and Blade Row Stall in Axial-flow Compressors written by Merle C. Huppert and published by . This book was released on 1952 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John R. Erwin
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.3/5 (91 download)
Download or read book Investigation of an Impulse Axial-flow Compressor written by John R. Erwin and published by . This book was released on 1950 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Merle C. Huppert
Publisher :
ISBN 13 :
Total Pages : 47 pages
Book Rating : 4.:/5 (713 download)
Download or read book Investigation of a 10-stage Subsonic Axial-flow Research Compressor written by Merle C. Huppert and published by . This book was released on 1953 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of rotating stall and surge at low and indeterminate speeds was conducted on a 10-stage subsonic axial-flow research compressor. The fluctuations of rotating stall and surge were detected by hot-wire anemometers and pressure transducers.
Author : Nasa Technical Reports Server (Ntrs)
Publisher : BiblioGov
ISBN 13 : 9781289094416
Total Pages : 24 pages
Book Rating : 4.0/5 (944 download)
Download or read book Investigation of Performance of Axial-Flow Compressor of Xt-46 Turbine-Propeller Engine written by Nasa Technical Reports Server (Ntrs) and published by BiblioGov. This book was released on 2013-06 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation is being conducted to determine the performance of the 12-stage axial-flow compressor of the XT-46 turbine-propeller engine. This compressor was designed to produce a pressure ratio of 9 at an adiabatic efficiency of 0.86. The design pressure ratios per stage were considerably greater than any employed in current aircraft gas-turbine engines using this type of compressor. The compressor performance was evaluated at two stations. The station near the entrance section of the combustors indicated a peak pressure ratio of 6.3 at an adiabatic efficiency of 0.63 for a corrected weight flow of 23.1 pounds per second. The other, located one blade-chord downstream of the last stator row, indicated a peak pressure ratio of 6.97 at an adiabatic efficiency of 0.81 for a corrected weight flow of 30.4 pounds per second. The difference in performance obtained at the two stations is attributed to shock waves in the vicinity of the last stator row. These shock waves and the accompanying flow choking, together with interstage circulatory flows, shift the compressor operating curves into the region where surge would normally occur. The inability of the compressor to meet design pressure ratio is probably due to boundary-layer buildup in the last stages, which cause axial velocities greater than design values that, in turn, adversely affect the angles of attack and turning angles in these blade rows.
Author : Eyad H. Abed
Publisher :
ISBN 13 :
Total Pages : 8 pages
Book Rating : 4.:/5 (248 download)
Download or read book Bifurcation Analysis of Surge and Rotating Stall in Axial Flow Compressors written by Eyad H. Abed and published by . This book was released on 1990 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt: These results are used to reconstruct Greitzer's (1976) findings regarding the manner in which post-instability behavior depends on system parameters. Moreover, the results provide significant new insight deemed valuable in the prediction, analysis and control of stall instabilities in gas turbine jet engines."
Author : Robert O. Bullock
Publisher :
ISBN 13 :
Total Pages : 552 pages
Book Rating : 4.:/5 (317 download)
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:
Author : Irving A. Johnsen
Publisher :
ISBN 13 :
Total Pages : 41 pages
Book Rating : 4.:/5 (11 download)
Download or read book Investigation of a 10-stage Subsonic Axial-flow Research Compressor written by Irving A. Johnsen and published by . This book was released on 1952 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt:
