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Elementary Two Dimensional Considerations In The Design Of A Supersonic Axial Flow Compressor
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Book Synopsis Elementary, Two-dimensional, Considerations in the Design of a Supersonic, Axial-flow, Compressor by : Gerald Sylvester Healy
Download or read book Elementary, Two-dimensional, Considerations in the Design of a Supersonic, Axial-flow, Compressor written by Gerald Sylvester Healy and published by . This book was released on 1958 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Design of Axial-flow Compressors by : Lewis Research Center
Download or read book Aerodynamic Design of Axial-flow Compressors written by Lewis Research Center and published by . This book was released on 1965 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Design of Axial Flow Compressors by : Robert O. Bullock
Download or read book Aerodynamic Design of Axial Flow Compressors written by Robert O. Bullock and published by . This book was released on 1965 with total page 552 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Performance of Supersonic Axial-flow Compressors Based on One-dimensional Analysis by : Linwood C. Wright
Download or read book Performance of Supersonic Axial-flow Compressors Based on One-dimensional Analysis written by Linwood C. Wright and published by . This book was released on 1949 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Axial-flow Compressors by : Ronald H. Aungier
Download or read book Axial-flow Compressors written by Ronald H. Aungier and published by American Society of Mechanical Engineers. This book was released on 2003 with total page 386 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Series of Articles on Compressor and Fan Design Written by German Engineers: Basic considerations in the design of axial flow compressors by : United States. Navy Dept. Bureau of Ships
Download or read book Series of Articles on Compressor and Fan Design Written by German Engineers: Basic considerations in the design of axial flow compressors written by United States. Navy Dept. Bureau of Ships and published by . This book was released on 1946 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Axial Flow Compressor by : Edward M. Rex
Download or read book An Axial Flow Compressor written by Edward M. Rex and published by . This book was released on 1956 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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
Download or read book 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 written by Willard R. Westphal and published by . This book was released on 1958 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Application of Supersonic Flow Theory to the Design of Two-dimensional Supersonic Impulse Compressor and Turbine Blade Sections by : Emanuel Boxer
Download or read book Application of Supersonic Flow Theory to the Design of Two-dimensional Supersonic Impulse Compressor and Turbine Blade Sections written by Emanuel Boxer and published by . This book was released on 1951 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamics of Turbines and Compressors. (HSA-1), Volume 1 by : William R. Hawthorne
Download or read book Aerodynamics of Turbines and Compressors. (HSA-1), Volume 1 written by William R. Hawthorne and published by Princeton University Press. This book was released on 2017-03-14 with total page 647 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Analysis of the Effects of Design Pressure Ratio Per Stage and Off-design Efficiency on the Operating Range of Multistage Axial-flow Compressors by : Melvyn Savage
Download or read book Analysis of the Effects of Design Pressure Ratio Per Stage and Off-design Efficiency on the Operating Range of Multistage Axial-flow Compressors written by Melvyn Savage and published by . This book was released on 1950 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Multistage compressors composed of high-pressure-ratio stages have higher over-all off-design efficiencies and a wider operating range than those made up of low-pressure-ratio stages if the blade-row efficiency curves for the two cases are assumed to be somewhat similar.
Book Synopsis Some Methods of Analyzing the Effect of Basic Design Variables on Axial-flow-compressor Performance by : John T. Sinnette (Jr.)
Download or read book Some Methods of Analyzing the Effect of Basic Design Variables on Axial-flow-compressor Performance written by John T. Sinnette (Jr.) and published by . This book was released on 1947 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Reference Publication written by and published by . This book was released on 1977 with total page 944 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Basic Considerations in the Design of Axial Flow Compressors by : Fritz Weinig
Download or read book Basic Considerations in the Design of Axial Flow Compressors written by Fritz Weinig and published by . This book was released on 1946 with total page 79 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis On Two-dimensional Supersonic Flows by : Stefan Bergman
Download or read book On Two-dimensional Supersonic Flows written by Stefan Bergman and published by . This book was released on 1949 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: In previous reports by the author, the method of operators has been applied to investigation of two-dimensional flow patterns of an ideal compressible fluid, mostly in the subsonic case. Using a similar approach in the present paper, the author defines two different operators which generate supersonic two-dimensional flow patterns from differentiable functions of one real variable. (An operator is any rul by means of which one function is converted into another.) Since operators of the type considered preserve many properties of the functions to which they are applied and since the theory of functions of one real variable is more extensively developed than that of solutions of the compressibility equations, the results can be used as a basis for investigation of supersonic flow patterns.
Book Synopsis Supersonic Axial Velocity Compressor Study. Volume Iv. Two-dimensional Cascade Test Results by : F. W. Lipfert
Download or read book Supersonic Axial Velocity Compressor Study. Volume Iv. Two-dimensional Cascade Test Results written by F. W. Lipfert and published by . This book was released on 1967 with total page 109 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume presents a description of the cascade tests conducted to establish feasibility of the supersonic axial velocity compressor concept. Two series of tests were conducted at a free stream Mach number of 2.7 using a cascade of four two-dimensional impulse blades, having about 60 deg. turning. The blade profile was modified slightly for the second test series to alleviate suction surface boundary layer separation. The angle of attack of the cascade was varied roughly plus or minus 15 deg. Measurements consisted of pressure distributions along the blade surfaces and the total pressure recovery at the passage exit. The maximum mass-weighted recovery was 80%. (Author).
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:
