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A Theoretical Investigation Of Some Design Variables For The Supersonic Axialflow Compressor
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Book Synopsis A Theoretical Investigation of Some Design Variables for the Supersonic, Axialflow Compressor by : Hugh B. Thompson
Download or read book A Theoretical Investigation of Some Design Variables for the Supersonic, Axialflow Compressor written by Hugh B. Thompson and published by . This book was released on 1948 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of an Axial-flow Supersonic Compressor Having Sharp Leading-edge Blades with an 8-percent Mean Thickness-chord Ratio by : Theodore J. Goldberg
Download or read book Experimental Investigation of an Axial-flow Supersonic Compressor Having Sharp Leading-edge Blades with an 8-percent Mean Thickness-chord Ratio written by Theodore J. Goldberg and published by . This book was released on 1955 with total page 38 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 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:
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 Investigation of an Experimental Supersonic Axial-flow Compressor by : John R. Erwin
Download or read book Investigation of an Experimental Supersonic Axial-flow Compressor written by John R. Erwin and published by . This book was released on 1947 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Study of a Supersonic Axial Flow Compressor by : Wu-Wai Chao
Download or read book A Study of a Supersonic Axial Flow Compressor written by Wu-Wai Chao and published by . This book was released on 1949 with total page 424 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 A Study of Off-design Performance of an Axial Flow Compressor by : William Brenton Noé
Download or read book A Study of Off-design Performance of an Axial Flow Compressor written by William Brenton Noé and published by . This book was released on 1954 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis ˜Aœ Theoretical Investigation of the Effect of Aspects Ratio on Axial Flow Compressor Performance by : John H. Horlock
Download or read book ˜Aœ Theoretical Investigation of the Effect of Aspects Ratio on Axial Flow Compressor Performance written by John H. Horlock and published by . This book was released on 1967 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of a Shrouded and an Unshrouded Axial-flow Supersonic Compressor by : Emanuel Boxer
Download or read book Investigation of a Shrouded and an Unshrouded Axial-flow Supersonic Compressor written by Emanuel Boxer and published by . This book was released on 1950 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Theoretical Investigations on the General Flow Patterns in Axial Flow Compressors by : Rolf H. Sabersky
Download or read book Experimental and Theoretical Investigations on the General Flow Patterns in Axial Flow Compressors written by Rolf H. Sabersky and published by . This book was released on 1949 with total page 350 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of an Axial-flow Supersonic Compressor Having Rounded Leading-edge Blades with an 8-percent Mean Thickness-chord Ratio by : Theodore J. Goldberg
Download or read book Experimental Investigation of an Axial-flow Supersonic Compressor Having Rounded Leading-edge Blades with an 8-percent Mean Thickness-chord Ratio written by Theodore J. Goldberg and published by . This book was released on 1953 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of a One Stage Axial Flow Supersonic Compressor, Part 2. Blade Section Performance of the Blunt Trailing Edge Rotor R-32 by : Fr Breugelmans
Download or read book Investigation of a One Stage Axial Flow Supersonic Compressor, Part 2. Blade Section Performance of the Blunt Trailing Edge Rotor R-32 written by Fr Breugelmans and published by . This book was released on 1965 with total page 85 pages. Available in PDF, EPUB and Kindle. Book excerpt: A high pressure ratio, supersonic axial flow compressor was investigated in a range of relative inlet Mach numbers at tip radius of the rotor from 0.66 to 1.45. The compressor blading was the blunt trailing edge blade. All tests were made by using a Freon-12 + air (20%) atmosphere because of power and speed limitations. Part II describes the blade sections performance, flow angle and velocity distribution and diffusion parameters. All data discussed concern measurements in a plane one axial chord downstream the rotor, which is tested without inlet guide vanes and without stator. (Author).
Book Synopsis Preliminary Analysis of Axial-flow Compressors Having Supersonic Velocity at the Entrance of the Stator by : Antonio Ferri
Download or read book Preliminary Analysis of Axial-flow Compressors Having Supersonic Velocity at the Entrance of the Stator written by Antonio Ferri and published by . This book was released on 1949 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Supersonic Axial-flow Compressor by : Arthur Kantrowitz
Download or read book The Supersonic Axial-flow Compressor written by Arthur Kantrowitz and published by . This book was released on 1946 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of the Flow Field in a Transonic, Axial Flow Compressor with Respect to the Development of Blockage and Loss by : Kenneth Lee Suder
Download or read book Experimental Investigation of the Flow Field in a Transonic, Axial Flow Compressor with Respect to the Development of Blockage and Loss written by Kenneth Lee Suder and published by . This book was released on 1996 with total page 272 pages. Available in PDF, EPUB and Kindle. Book excerpt:
