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Author : John R. Erwin
Publisher :
ISBN 13 :
Total Pages : 33 pages
Book Rating : 4.:/5 (7 download)
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:
Author : Theodore J. Goldberg
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.3/5 (91 download)
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:
Author : Theodore J. Goldberg
Publisher :
ISBN 13 :
Total Pages : 43 pages
Book Rating : 4.:/5 (11 download)
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:
Author : Linwood C. Wright
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.3/5 (91 download)
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:
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722219574
Total Pages : 32 pages
Book Rating : 4.2/5 (195 download)
Download or read book Experimental Investigation of the Performance of a Supersonic Compressor Cascade written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-03 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are presented from an experimental investigation of a linear, supersonic, compressor cascade tested in the supersonic cascade wind tunnel facility at the DFVLR in Cologne, Federal Republic of Germany. The cascade design was derived from the near-tip section of a high-through-flow axial flow compressor rotor with a design relative inlet Mach number of 1.61. Test data were obtained over a range of inlet Mach numbers from 1.23 to 1.71, and a range of static pressure ratios and axial-velocity-density ratios (AVDR) at the design inlet condition. Flow velocity measurements showing the wave pattern in the cascade entrance region were obtained using a laser transit anemometer. From these measurements, some unique-incidence conditions were determined, thus relating the supersonic inlet Mach number to the inlet flow direction. The influence of static pressure ratio and AVDR on the blade passage flow and the blade-element performance is described, and an empirical correlation is used to show the influence of these two (independent) parameters on the exit flow angle and total-pressure loss for the design inlet condition. Tweedt, D. L. and Schreiber, H. A. and Starken, H. Glenn Research Center RTOP 505-62-61...
Author : Kenneth Lee Suder
Publisher :
ISBN 13 :
Total Pages : 272 pages
Book Rating : 4.:/5 (317 download)
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:
Author : Wolfgang Elmendorf
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (137 download)
Download or read book Design and Experimental Investigation of a Mixed Flow Supersonic Compressor Stage written by Wolfgang Elmendorf and published by . This book was released on 1995 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented at the International Gas Turbine and Aeroengine Congress and Exposition, Houston, Texas - June 5-8, 1995.
Author : Sanford Fleeter
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (227 download)
Download or read book Experimental Investigation of a Supersonic Compressor Cascade written by Sanford Fleeter and published by . This book was released on 1975 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes in detail the experimental investigation of a stationary, linear, supersonic compressor cascade with blades of constant spanwise geometry and constant thickness linear sidewalls. The selected blade element was representative of streamline 19 of an advanced compressor configuration resulting from the Aerospace Research Laboratories axial compressor research program. The investigation covered the range of inlet relative Mach numbers of 1.535 - 1.683 and a range of static pressure ratios of approximately 1.1 - 2.3 and included laser velocimeter measurements of the flow within and around the cascade at the design Mach number.
Author : S. A. T. Stoneman
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (52 download)
Download or read book An Experimental Investigation of Flow Excited Acoustic Fields in an Axial Flow Compressor written by S. A. T. Stoneman and published by . This book was released on 1984 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John R. Erwin
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.3/5 (91 download)
Download or read book Investigation of an Impulse Axial-flow Compressor written by John R. Erwin and published by . This book was released on 1950 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Sanford Fleeter
Publisher :
ISBN 13 :
Total Pages : 338 pages
Book Rating : 4.3/5 (91 download)
Download or read book Experimental Investigation of a Supersonic Compressor Cascade written by Sanford Fleeter and published by . This book was released on 1975 with total page 338 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes in detail the experimental investigation of a stationary, linear, supersonic compressor cascade with blades of constant spanwise geometry and constant thickness linear sidewalls. The selected blade element was representative of streamline 19 of an advanced compressor configuration resulting from the Aerospace Research Laboratories axial compressor research program. The investigation covered the range of inlet relative Mach numbers of 1.535 - 1.683 and a range of static pressure ratios of approximately 1.1 - 2.3 and included laser velocimeter measurements of the flow within and around the cascade at the design Mach number.
Author : Emanuel Boxer
Publisher :
ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.:/5 (7 download)
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:
Author : Charles C. Alsworth
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (159 download)
Download or read book Theoretical and Experimental Investigations of Axial Flow Compressors ... written by Charles C. Alsworth and published by . This book was released on 1900 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 226 pages
Book Rating : 4.:/5 (318 download)
Download or read book Material Presented at the Conference on Compressor Research at Aircraft Engine Research Laboratory on September 11, 1946 written by and published by . This book was released on 1946 with total page 226 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : William R. Hawthorne
Publisher : Princeton University Press
ISBN 13 : 1400885981
Total Pages : 647 pages
Book Rating : 4.4/5 (8 download)
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.
Author : Donald M. Sandercock
Publisher :
ISBN 13 :
Total Pages : 35 pages
Book Rating : 4.:/5 (697 download)
Download or read book Experimental Investigation of a Five-stage Axial-flow Research Compressor with Transonic Rotors in All Stages written by Donald M. Sandercock and published by . This book was released on 1954 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Luke L. Liccini
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.3/5 (91 download)
Download or read book Experimental Investigation of the Mixing Loss Behind Trailing Edge of a Cascade of Three 90© Supersonic Turning Passages written by Luke L. Liccini and published by . This book was released on 1950 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
