Axial Flow Compressors

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Axial-flow Compressors

Author : Ronald H. Aungier
Publisher : American Society of Mechanical Engineers
Page : 386 pages
File Size : 49,5 Mb
Release : 2003
Category : Science
ISBN : UOM:39015052660845

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Axial-flow Compressors by Ronald H. Aungier Pdf

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.

Aerodynamic Design of Axial-flow Compressors

Author : Lewis Research Center
Publisher : Unknown
Page : 542 pages
File Size : 50,6 Mb
Release : 1965
Category : Axial flow compressors
ISBN : STANFORD:36105113764901

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Aerodynamic Design of Axial-flow Compressors by Lewis Research Center Pdf

Aerodynamic Design of Axial Flow Compressors

Author : Robert O. Bullock
Publisher : Unknown
Page : 552 pages
File Size : 50,8 Mb
Release : 1965
Category : Axial flow compressors
ISBN : NASA:31769000652464

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Aerodynamic Design of Axial Flow Compressors by Robert O. Bullock Pdf

Design and Tests of a Six-stage Axial-flow Compressor Having a Tip Speed of 550 Feet Per Second and a Flat Operating Characteristic at Constant Speed

Author : Willard R. Westphal,John W. Maynard
Publisher : Unknown
Page : 66 pages
File Size : 47,9 Mb
Release : 1958
Category : Axial flow compressors
ISBN : UOM:39015086414565

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Design and Tests of a Six-stage Axial-flow Compressor Having a Tip Speed of 550 Feet Per Second and a Flat Operating Characteristic at Constant Speed by Willard R. Westphal,John W. Maynard Pdf

A six-stage axial-flow compressor with a tip speed of 550 feet per second and a flat operating characteristics at constant speed has been designed and tested. It was designed for a constant power input per pound of flow in expectation that this would result in a wider mass-flow operating range at a given stagnation-presssure ratio. The design specific weight flow was 21.3 pounds per second per square foot of frontal area at atmospheric discharge with a stagnation-pressure ratio of 3.25 and an inlet hub-tip radius ratio of 0.7. Several configurations consisting of various blade setting angles and solidities were tested. Tests showed that the design flow, pressure ratio, and flat operating characteristic were obtained over a range of 10 percent of design flow at a peak efficiency of 82 percent for design conditions. The compressor had a possible immediate application for air removal from a large slotted-throat transonic wind tunnel, but the design theory could apply to any low-speed industrial compressor or second spool of a turbojet engine.

Standard Procedures for Rating and Testing Multistage Axial-flow Compressors

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 544 pages
File Size : 45,8 Mb
Release : 1946
Category : Axial flow compressors
ISBN : STANFORD:36105024795366

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Standard Procedures for Rating and Testing Multistage Axial-flow Compressors by United States. National Advisory Committee for Aeronautics Pdf

In order to establish a standard procedure for rating and testing multistage axial-flow compressors, the NACA Subcommittee on Compressors appointed a panel to write such a procedure. This panel made recommendations for standardization of test setups, instrumentation, test procedure, data to be taken, and the presentation of the data. These recommendations are presented.

Aerodynamic Design of Axial-flow Compressors

Author : Lewis Research Center
Publisher : Unknown
Page : 128 pages
File Size : 41,5 Mb
Release : 1956
Category : Axial flow compressors
ISBN : OCLC:637013917

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Aerodynamic Design of Axial-flow Compressors by Lewis Research Center Pdf

Axial Flow Fans and Compressors

Author : A. B. McKenzie
Publisher : Ashgate Publishing
Page : 290 pages
File Size : 40,7 Mb
Release : 1997
Category : Science
ISBN : UOM:39015041356315

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Axial Flow Fans and Compressors by A. B. McKenzie Pdf

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.

An Investigation of the Dynamic Characteristics of Axial Flow Compressors

Author : Guo-Cai Tang,Bing Hu
Publisher : Unknown
Page : 0 pages
File Size : 41,8 Mb
Release : 1990
Category : Axial flow compressors
ISBN : OCLC:1426312791

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An Investigation of the Dynamic Characteristics of Axial Flow Compressors by Guo-Cai Tang,Bing Hu Pdf

This paper reports an experimental investigation of the dynamic behavior of an axial flow compressor when the flow rate if forced to vary quickly. The results are discussed in two aspects: general trends and special points. Generally, there is a deviation of the dynamic characteristic from the steady-state one, depending upon the algebraic sum of the inertial effect and the lag effect. For the present axial flow compressor, lightly-loaded, the dynamic characteristic goes above the steady-state one while closing the valve and below the steady-state one for opening the valve. Physical explanation is given to the general trend and also to the difference between the behavior of the axial flow compressor and that of the centrifugal compressor. Specifically, the rapid closing of the valve will end up with an operating point end dynamic breaking into the instability limit while the throttle setting is somewhat away from the instability limit position for steady-state operation; and the rapid opening of the valve may produce an initial transient decrease in flow rate thus may have an initial dynamic breaking into the instability limit. Physical explanation is also given to these two special points, which are of great engineering interest with regard to the instability issue.

Radial Flow Turbocompressors

Author : Michael Casey,Chris Robinson
Publisher : Cambridge University Press
Page : 789 pages
File Size : 47,9 Mb
Release : 2021-06-10
Category : Science
ISBN : 9781108416672

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Radial Flow Turbocompressors by Michael Casey,Chris Robinson Pdf

An introduction to the theory and engineering practice that underpins the component design and analysis of radial flow turbocompressors. Drawing upon an extensive theoretical background and years of practical experience, the authors provide descriptions of applications, concepts, component design, analysis tools, performance maps, flow stability, and structural integrity, with illustrative examples. Features wide coverage of all types of radial compressor over many applications unified by the consistent use of dimensional analysis. Discusses the methods needed to analyse the performance, flow, and mechanical integrity that underpin the design of efficient centrifugal compressors with good flow range and stability. Includes explanation of the design of all radial compressor components, including inlet guide vanes, impellers, diffusers, volutes, return channels, de-swirl vanes and side-streams. Suitable as a reference for advanced students of turbomachinery, and a perfect tool for practising mechanical and aerospace engineers already within the field and those just entering it.

Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory

Author : John T. Sinnette,Oscar W. Schey,J. Austin King
Publisher : Unknown
Page : 74 pages
File Size : 47,7 Mb
Release : 1944
Category : Aerofoils
ISBN : UOM:39015095014299

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Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory by John T. Sinnette,Oscar W. Schey,J. Austin King Pdf

The NACA has conducted an investigation to determine the performance that can be obtained from a multistage axial-flow compressor based on airfoil research. A theory was developed; an eight-stage axial-flow compressor was designed, constructed, and tested.

Aerodynamics of Turbines and Compressors. (HSA-1), Volume 1

Author : William R. Hawthorne
Publisher : Princeton University Press
Page : 646 pages
File Size : 43,9 Mb
Release : 2017-03-14
Category : Technology & Engineering
ISBN : 9781400885985

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Aerodynamics of Turbines and Compressors. (HSA-1), Volume 1 by William R. Hawthorne Pdf

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.