"Compressor Instability with Integral Methods" is a book, to bring together the quick integral approaches and advances in the field for the prediction of stall and surge problem in compre… Mehr…
"Compressor Instability with Integral Methods" is a book, to bring together the quick integral approaches and advances in the field for the prediction of stall and surge problem in compressor. This book is useful for people involved in the flow analysis, design and testing of rotating machinery. For students, it can be used as a specialized topic of senior undergraduate or graduate study. The book can also be served as a self-study material to those who keen to acquire this knowledge. In brief, this book focuses on the numerical/computational analysis for the effect of distorted inlet flow propagation on the rotating stall and surge in axial compressors. It gains insight into the basic phenomena controlling these flow instabilities, and reveals the influence of inlet parameters on rotating stall and surge. The book starts from the confirmation and application of Kim et al's integral method and then follows by a development to this method through the proposing and applying a critical distortion line. This line is applied successfully on the stall prediction of in-flight compressor due to flamming of refueling leakage near inlet, a typical real and interesting example of compressor stall and surge operation. Further, after a parametric study on the integral method and the distorted flow field of compressor using Taguchi method, a novel integral method is formulated using more appropriate and practical airfoil characteristics, with a less assumptions needed for derivation. Finally, as an extended work, the famous Greitzer's instability flow model, the well-known B-parameter model applied for analyzing the stall and surge characteristics, is studied parametrically using Taguchi method., Springer<
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Nr. 978-3-540-72411-7. Versandkosten:Worldwide free shipping, , DE. (EUR 0.00) Details...
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[EAN: 9783540724117], Neubuch, [PU: Springer Berlin Heidelberg], INTEGRATION (MATHEMATISCH) NUMERIK (NATURWISSENSCHAFTLICH, EDV) MECHANIK STRöMUNGSMECHANIK TECHNISCHE FOURTH-ORDERRUNGE-KUTTAMETHOD GREITZER\\'SB-PARAMETERMODEL INLETFLOWPROPAGATION CONTROL DESIG TECHNIK MASCHINENBAU FERTIGUNGSTECHNIK, Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Hot topic for Practitioners and Designers in Mechanical and Aeronautical Engineering Treat distortion und stall in turbines This book brings together the quick integral approaches and advances in the field for the prediction of stall an., Books<
Hard cover, New., Sewn binding. Paper over boards. 134 p. Contains: Unspecified, Illustrations, black & white, Tables, black & white., Berlin, Heidelberg, [PU: Springer]
"Compressor Instability with Integral Methods" is a book, to bring together the quick integral approaches and advances in the field for the prediction of stall and surge problem in compre… Mehr…
"Compressor Instability with Integral Methods" is a book, to bring together the quick integral approaches and advances in the field for the prediction of stall and surge problem in compressor. This book is useful for people involved in the flow analysis, design and testing of rotating machinery. For students, it can be used as a specialized topic of senior undergraduate or graduate study. The book can also be served as a self-study material to those who keen to acquire this knowledge. In brief, this book focuses on the numerical/computational analysis for the effect of distorted inlet flow propagation on the rotating stall and surge in axial compressors. It gains insight into the basic phenomena controlling these flow instabilities, and reveals the influence of inlet parameters on rotating stall and surge. The book starts from the confirmation and application of Kim et al's integral method and then follows by a development to this method through the proposing and applying a critical distortion line. This line is applied successfully on the stall prediction of in-flight compressor due to flamming of refueling leakage near inlet, a typical real and interesting example of compressor stall and surge operation. Further, after a parametric study on the integral method and the distorted flow field of compressor using Taguchi method, a novel integral method is formulated using more appropriate and practical airfoil characteristics, with a less assumptions needed for derivation. Finally, as an extended work, the famous Greitzer's instability flow model, the well-known B-parameter model applied for analyzing the stall and surge characteristics, is studied parametrically using Taguchi method., Springer<
Nr. 978-3-540-72411-7. Versandkosten:Worldwide free shipping, , DE. (EUR 0.00)
[EAN: 9783540724117], Neubuch, [PU: Springer Berlin Heidelberg], INTEGRATION (MATHEMATISCH) NUMERIK (NATURWISSENSCHAFTLICH, EDV) MECHANIK STRöMUNGSMECHANIK TECHNISCHE FOURTH-ORDERRUNGE-KUTTAMETHOD GREITZER\\'SB-PARAMETERMODEL INLETFLOWPROPAGATION CONTROL DESIG TECHNIK MASCHINENBAU FERTIGUNGSTECHNIK, Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Hot topic for Practitioners and Designers in Mechanical and Aeronautical Engineering Treat distortion und stall in turbines This book brings together the quick integral approaches and advances in the field for the prediction of stall an., Books<
Hard cover, New., Sewn binding. Paper over boards. 134 p. Contains: Unspecified, Illustrations, black & white, Tables, black & white., Berlin, Heidelberg, [PU: Springer]
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This book brings together the quick integral approaches and advances in the field for the prediction of stall and surge problems in the compressor. The book is useful for people involved in the flow analysis, design and testing of rotating machinery. For students, it can be used as a specialized topic of senior undergraduate or graduate study. The book can also serve as self-study material.
Detailangaben zum Buch - Mapping the Management Journey: Practice, Theory, and Context
EAN (ISBN-13): 9783540724117 ISBN (ISBN-10): 3540724117 Gebundene Ausgabe Taschenbuch Erscheinungsjahr: 2007 Herausgeber: Dopson, Sue, Earl, Michael, Snow, Peter, Oxford University Press 134 Seiten Gewicht: 0,362 kg Sprache: eng/Englisch
Buch in der Datenbank seit 2007-05-17T11:35:48+02:00 (Zurich) Detailseite zuletzt geändert am 2024-02-25T07:51:55+01:00 (Zurich) ISBN/EAN: 3540724117
ISBN - alternative Schreibweisen: 3-540-72411-7, 978-3-540-72411-7 Alternative Schreibweisen und verwandte Suchbegriffe: Autor des Buches: liu, michael snow, greitzer Titel des Buches: instabil, instability, integral, ngü, green ethics metaphysics and political philosophy, eddie
Daten vom Verlag:
Autor/in: Eddie Y.K. Ng Titel: Compressor Instability with Integral Methods Verlag: Springer; Springer Berlin 134 Seiten Erscheinungsjahr: 2007-08-08 Berlin; Heidelberg; DE Sprache: Englisch 109,99 € (DE)
Study on the Propagation of Inlet Flow Distortion in Axial Compressor Using an Integral Method.- Stall Prediction of In-flight Compressor due to Flaming of Refueling Leakage near Inlet.- Parametric Study of Inlet Distortion Propagation in Compressor with Integral Approach and Taguchi Method.- A Development of Novel Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor.- Parametric Study of Greitzer’s Instability Flow Model Through Compressor System Using Taguchi Method.
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