Author: Saju Thomas JosephPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 228
Book Description
Effect of Compressor Parameters on Rotating Stall
Author: Saju Thomas JosephPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 228
Book Description
Effect of Cascade Parameters on Rotating Stall [with List of References]
![Effect of Cascade Parameters on Rotating Stall [with List of References] PDF](https://books.google.com/books/content/images/frontcover/fA60YgEACAAJ?fife=w80-h100)
Author: Publisher:
ISBN:
Category : Cascades (Fluid dynamics)
Languages : en
Pages : 33
Book Description
Compressor Surge and Rotating Stall
Author: Jan Tommy GravdahlPublisher: Springer Science & Business Media
ISBN: 1447108272
Category : Technology & Engineering
Languages : en
Pages : 233
Book Description
The series Advances in Industrial Control aims to report and encourage technology transfer in control engineering. The rapid development of control technology impacts all areas of the control discipline. New theory, new controllers, actuators, sensors, new industrial processes, computer methods, new applications, new philosophies . . . , new challenges. Much of this development work resides in industrial reports, feasibility study papers and the reports of advanced collaborative projects. The series offers an opportunity for researchers to present an extended exposition of such new work in all aspects of industrial control for wider and rapid dissemination. Operating plant as close as possible to constraint boundaries so often brings economic benefits in industrial process control. This is the conundrum at the heart of this monograph by Tommy Gravdahl and Olav Egeland on stall control for compressors. Operation of the compressor closer to the surge line can increase operational efficiency and flexibility The approach taken by the authors follows the modern control system paradigm: -physical understanding, detailed modelling and simulation studies and finally control studies. The thoroughness of the presentation, bibliography and appendices indicates that the volume has all the hallmarks of being a classic for its subject. Despite the monograph's narrow technical content, the techniques and insights presented should appeal to the wider industrial control community as well as the gas turbine/compressor specialist. M. J. Grimble and M. A.
Compressor Instability with Integral Methods
Author: Eddie Y.K. NgPublisher: Springer Science & Business Media
ISBN: 3540724125
Category : Technology & Engineering
Languages : en
Pages : 154
Book Description
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.
Rotating Stall in Centrifugal Compressor and Its Effect on Inducing Vibration
Author: Abraham EngedaDynamic Control of Rotating Stall in Axial Flow Compressors Using Aeromechanical Feedback
Author: Daniel L. GyslingPublisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 347
Book Description
Compressor Surge and Stall
Author: R. C. PampreenPublisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 532
Book Description
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].
Analytical and Experimental Investigation of Rotating Stall Phenomena in Turbine Engine Compressors
Author: A Theory of Rotating Stall of Multistage Axial Compressors
Author: Franklin K. MoorePublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 96
Book Description
Compressibility Effects on Rotating Stall in a Two-stage Axial Compressor
Author: Jaideep Sahai MathurPublisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 150
Book Description