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Author : Lewis Research Center
Publisher : Unknown
Page : 542 pages
File Size : 51,6 Mb
Release : 1965
Category : Axial flow compressors
ISBN : STANFORD:36105113764901
Author : Ronald H. Aungier
Publisher : American Society of Mechanical Engineers
Page : 386 pages
File Size : 52,8 Mb
Release : 2003
Category : Science
ISBN : UOM:39015052660845
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 : Robert O. Bullock
Publisher : Unknown
Page : 552 pages
File Size : 53,7 Mb
Release : 1965
Category : Axial flow compressors
ISBN : NASA:31769000652464
Author : Lewis Research Center
Publisher : Unknown
Page : 128 pages
File Size : 47,5 Mb
Release : 1956
Category : Axial flow compressors
ISBN : OCLC:637013917
Author : Irving A. Johnsen,Robert O. Bullock
Publisher : Unknown
Page : 128 pages
File Size : 52,9 Mb
Release : 1956
Category : Axial flow compressors
ISBN : OCLC:222185400
Author : A. B. McKenzie
Publisher : Ashgate Publishing
Page : 290 pages
File Size : 48,6 Mb
Release : 1997
Category : Science
ISBN : UOM:39015041356315
Provides readers with an understanding of aerodynamic design and performance of fans and compressors. The book includes practical emphasis on design problems, experimental facilities and data analysis, together with some design examples and novel concepts.
Author : William R. Hawthorne
Publisher : Princeton University Press
Page : 646 pages
File Size : 52,9 Mb
Release : 2017-03-14
Category : Technology & Engineering
ISBN : 9781400885985
Volume X of the High Speed Aerodynamics and Jet Propulsion series. Contents include: Theory of Two-Dimensional Flow through Cascades; Three-Dimensional Flow in Turbomachines; Experimental Techniques; Flow in Cascades; The Axial Compressor Stage; The Supersonic Compressor; Aerodynamic Design of Axial Flow Turbines; The Radial Turbine; The Centrifugal Compressor; Intermittent Flow Effects. Originally published in 1964. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author : Ronald H. Aungier
Publisher : American Society of Mechanical Engineers
Page : 336 pages
File Size : 44,9 Mb
Release : 2000
Category : Science
ISBN : UOM:39015048532652
A mechanical engineer with a Pennsylvania turbomachinery company, A ungier describes his own system and strategy for designing and analyzing centrifugal compressor aerodynamics. To address the novice as well as the experienced in the field, he presents the basic thermodynamic and fluid dynamic principles, empirical models, and key numerical methods that form the basis of his methods. His strategy, or design practice, he found harder to describe because it involves a process of reasoning rather than following an established set of principles. He recognizes that his is only one of many possible methods, but makes no effort to compare or contrast his with any other.
Author : Ronald H. Aungier
Publisher : American Society of Mechanical Engineers
Page : 424 pages
File Size : 52,6 Mb
Release : 2006
Category : Technology & Engineering
ISBN : UOM:39015064776423
This book provides a thorough description of actual, working aerodynamic design and analysis systems, for both axial-flow and radial-flow turbines. 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 type of aerodynamic design or analysis activity for both types of turbine. The book includes sufficient detail for readers to implement all or part of the systems. The author provides practical and effective design strategies for applying both turbine types, which are illustrated by design examples. Comparisons with experimental results are included to demonstrate the prediction accuracy to be expected. This book is intended for practicing engineers concerned with the design and development of turbines and related machinery.
Author : William R. Hawthorne
Publisher : Unknown
Page : 128 pages
File Size : 43,8 Mb
Release : 2017
Category : Compressors
ISBN : 1523124628
Author : National Aeronautics and Space Adm Nasa
Publisher : Unknown
Page : 96 pages
File Size : 54,9 Mb
Release : 2018-11-07
Category : Electronic
ISBN : 1730977308
An off-design axial-flow compressor code is presented and is available from COSMIC for predicting the aerodynamic performance maps of fans and compressors. Steady axisymmetric flow is assumed and the aerodynamic solution reduces to solving the two-dimensional flow field in the meridional plane. A streamline curvature method is used for calculating this flow-field outside the blade rows. This code allows for bleed flows and the first five stators can be reset for each rotational speed, capabilities which are necessary for large multistage compressors. The accuracy of the off-design performance predictions depend upon the validity of the flow loss and deviation correlation models. These empirical correlations for the flow loss and deviation are used to model the real flow effects and the off-design code will compute through small reverse flow regions. The input to this off-design code is fully described and a user's example case for a two-stage fan is included with complete input and output data sets. Also, a comparison of the off-design code predictions with experimental data is included which generally shows good agreement. Schmidt, James F. Unspecified Center...
Author : W.H.T. Loh
Publisher : Springer Science & Business Media
Page : 770 pages
File Size : 43,8 Mb
Release : 2012-12-06
Category : Technology & Engineering
ISBN : 9783642461095
During the last decade, rapid growth of knowledge in the field of jet, rocket, nuclear, ion and electric propulsion has resulted in many advances useful to the student, engineer and scientist. The purpose for offering this course is to make available to them these recent advances in theory and design. Accordingly, this course is organized into seven parts: Part 1 Introduction; Part 2 Jet Propulsion; Part 3 Rocket Propulsion; Part 4 Nuclear Propulsion; Part 5 Electric and Ion Propulsion; Part 6 Theory on Combustion, Detonation and Fluid Injection; Part 7 Advanced Concepts and Mission Applications. It is written in such a way that it may easily be adopted by other universities as a textbook for a one semester senior or graduate course on the subject. In addition to the undersigned who served as the course instructor and wrote Chapter I, 2 and 3, guest lecturers included: DR. G. L. DUGGER who wrote Chapter 4 "Ram-jets and Air-Aug mented Rockets," DR. GEORGE P. SUTTON who wrote Chapter 5 "Rockets and Cooling Methods," DR . . MARTIN SUMMERFIELD who wrote Chapter 6 "Solid Propellant Rockets," DR. HOWARD S. SEIFERT who wrote Chapter 7 "Hybrid Rockets," DR. CHANDLER C. Ross who wrote Chapter 8 "Advanced Nuclear Rocket Design," MR. GEORGE H. McLAFFERTY who wrote Chapter 9 "Gaseous Nuclear Rockets," DR. S. G. FORBES who wrote Chapter 10 "Electric and Ion Propul sion," DR. R. H. BODEN who wrote Chapter 11 "Ion Propulsion," DR.
Author : Zhengping Zou,Songtao Wang,Huoxing Liu,Weihao Zhang
Publisher : Springer
Page : 563 pages
File Size : 53,6 Mb
Release : 2018-01-11
Category : Technology & Engineering
ISBN : 9789811057502
This book is a monograph on aerodynamics of aero-engine gas turbines focusing on the new progresses on flow mechanism and design methods in the recent 20 years. Starting with basic principles in aerodynamics and thermodynamics, this book systematically expounds the recent research on mechanisms of flows in axial gas turbines, including high pressure and low pressure turbines, inter-turbine ducts and turbine rear frame ducts, and introduces the classical and innovative numerical evaluation methods in different dimensions. This book also summarizes the latest research achievements in the field of gas turbine aerodynamic design and flow control, and the multidisciplinary conjugate problems involved with gas turbines. This book should be helpful for scientific and technical staffs, college teachers, graduate students, and senior college students, who are involved in research and design of gas turbines.
Author : Kevin Wilkes
Publisher : Unknown
Page : 12 pages
File Size : 48,9 Mb
Release : 1996
Category : Electronic
ISBN : NASA:31769000614019
Presented at the International Gas Turbine and Aeroengine Congress & Exhibition Birmingham, UK - June 10-13, 1996.
Author : N. A. Cumpsty
Publisher : Longman Scientific and Technical
Page : 536 pages
File Size : 51,9 Mb
Release : 1989
Category : Technology & Engineering
ISBN : UOM:39015015531380
