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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 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 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 ˜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 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 Theoretical Investigation of the Effect of Aspect Ratio on Axial Flow Compressor Performance by : John Harold Horlock
Download or read book A Theoretical Investigation of the Effect of Aspect Ratio on Axial Flow Compressor Performance written by John Harold 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 Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1952 with total page 498 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.
Download or read book Report written by and published by . This book was released on 1945 with total page 620 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 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 1991 with total page 1460 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Download or read book Aeronautical Engineering written by and published by . This book was released on 1971 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Book Synopsis Experimental and Theoretical Investigation of Rotating-stall Characteristics of Single-stage Axial-flow Compressor with Hub-tip Ratio of 0.76 by : Robert W. Graham
Download or read book Experimental and Theoretical Investigation of Rotating-stall Characteristics of Single-stage Axial-flow Compressor with Hub-tip Ratio of 0.76 written by Robert W. Graham and published by . This book was released on 1953 with total page 34 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 A Selected Listing of NASA Scientific and Technical Reports for ... by :
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1949 with total page 750 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA SP. written by and published by . This book was released on 1988 with total page 624 pages. Available in PDF, EPUB and Kindle. Book excerpt:
