Compressor Instability with Integral Methods [electronic resource] / by Y.K. Eddie Ng, Ningyu Liu.

By: Eddie Ng, Y.K [author.]Contributor(s): Liu, Ningyu [author.] | SpringerLink (Online service)Material type: TextTextLanguage: English Publisher: Berlin, Heidelberg : Springer Berlin Heidelberg, 2007Description: XXIV, 133 p. 67 illus. online resourceContent type: text Media type: computer Carrier type: online resourceISBN: 9783540724124Subject(s): Engineering | Hydraulic engineering | Engineering | Engineering Fluid Dynamics | Numerical and Computational Methods in Engineering | Engineering Thermodynamics, Transport Phenomena | Machinery and Machine Elements | Automotive and Aerospace Engineering, TrafficAdditional physical formats: Printed edition:: No titleDDC classification: 620.1064 LOC classification: TA357-359Online resources: Click here to access online
Contents:
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.
In: Springer eBooksSummary: "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.
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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.

"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.

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