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Author : Hans Georg Mokelke
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (256 download)
Download or read book Circumferential inlet flow distortions in multi-stage axial compressors written by Hans Georg Mokelke and published by . This book was released on 1974 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : G. A. Plourde
Publisher :
ISBN 13 :
Total Pages : 11 pages
Book Rating : 4.:/5 (11 download)
Download or read book The Attenuation of Circumferential Inlet Distortion in Multi-stage Axial Compressors written by G. A. Plourde and published by . This book was released on 1967 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Frank R. Carter
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (325 download)
Download or read book Circumferential Inlet Distortions in an Axial Flow Compressor written by Frank R. Carter and published by . This book was released on 1958 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Roy D. Hager
Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (31 download)
Download or read book Analysis of Internal Flow of J85-13 Multistage Compressor written by Roy D. Hager and published by . This book was released on 1977 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : H. Mokelke
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book The Development of Inlet Flow Distortions in Multi-stage Axial Compressors of High-tip Ratio written by H. Mokelke and published by . This book was released on 1972 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Claude E. DeBogdan
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.F/5 ( download)
Download or read book Internal Flow Characteristics of a Multistage Compressor with Inlet Pressure Distortion written by Claude E. DeBogdan and published by . This book was released on 1977 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781721585243
Total Pages : 24 pages
Book Rating : 4.5/5 (852 download)
Download or read book Task IV written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-20 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: The concepts and the procedure developed in Task I and Task III were used to determine the response of an eleven-stage high-speed compressor to an inlet distortion of 180 deg. circumferential extent for contrasting against its performance under uniform inlet flow. Using the computed results at the inlet to and outlet of the compressor, the computed total pressure ratio and efficiency for the clean condition are determined to be 14.22 and 76.9 percent respectively. As for the distorted case, these are determined to be 10.35 and 71.8 percent respectively, showing deterioration 76.9 percent vs 71.8 percent). The physical consistency of the computed flow field was assessed as a means of demonstrating the applicability and utility of the body force representation for inlet distortion computations. Specifically the computed evolution of the distorted pattern in static pressure and total pressure from compressor inlet to exit is examined. For the eleven-stage compressor examined here, the deterioration in performance has been found to be particularly severe in the last 2 stages. This suggests that the last two stages could be redesigned to alleviate the observed deterioration thus making the compressor performance insensitive to circumferential inlet distortion. This can potentially be accomplished by first determining what should the body force distribution of the last two stages should be to achieve minimal or no deterioration in performance in the last two stages. One can then in principle proceed to determine the blade design to yield such a body force distribution. Tan, Choon-Sooi and Suder, Kenneth (Technical Monitor) Glenn Research Center
Author : Eddie Y.K. Ng
Publisher : Springer Science & Business Media
ISBN 13 : 3540724125
Total Pages : 154 pages
Book Rating : 4.5/5 (47 download)
Download or read book Compressor Instability with Integral Methods written by Eddie Y.K. Ng and published by Springer Science & Business Media. This book was released on 2007-07-07 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book brings together the quick integral approaches and advances in the field for the prediction of stall and surge problems in the compressor. The book is useful for people involved in the flow analysis, design and testing of rotating machinery. For students, it can be used as a specialized topic of senior undergraduate or graduate study. The book can also serve as self-study material.
Author : Jean Colpin
Publisher :
ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.F/5 ( download)
Download or read book Inlet Flow Distortions in Axial Flow Compressors written by Jean Colpin and published by . This book was released on 1977 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Marvin Stanley Shinbaum
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (326 download)
Download or read book Circumferential Distortion of the Inlet Flow in an Axial Compressor written by Marvin Stanley Shinbaum and published by . This book was released on 1959 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Zbigniew Krzywoblocki
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.3/5 (129 download)
Download or read book Compressibility Effects in Circumferential Inlet Distortion in Axial Compressors written by Zbigniew Krzywoblocki and published by . This book was released on 1958 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : William H. Robbins
Publisher :
ISBN 13 :
Total Pages : 105 pages
Book Rating : 4.:/5 (11 download)
Download or read book Experimental Investigation of the Effect of Circumferential Inlet Flow Distortion on the Performance of a Five-stage Axial-flow Research Compressor with Transonic Rotors in All Stages written by William H. Robbins and published by . This book was released on 1958 with total page 105 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Marvin S Shinbaum
Publisher : Hassell Street Press
ISBN 13 : 9781015039667
Total Pages : 118 pages
Book Rating : 4.0/5 (396 download)
Download or read book Circumferential Distortion of the Inlet Flow in an Axial Compressor. written by Marvin S Shinbaum and published by Hassell Street Press. This book was released on 2021-09-10 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt: This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Author : John E. Moss
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.F/5 ( download)
Download or read book Effect of Slotted Casing Treatment on Performance of a Multistage Compressor written by John E. Moss and published by . This book was released on 1976 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Ross Bakke Gridley
Publisher :
ISBN 13 :
Total Pages : 176 pages
Book Rating : 4.:/5 (677 download)
Download or read book Performance Characteristics of an Axial-flow Compressor Operating with Circumferential Inlet Flow Distortion written by Ross Bakke Gridley and published by . This book was released on 1980 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt:
![Download Internal Flow Characteristics of a Multistage Compressor with Inlet Pressure Distortion. [j85-13 Turbojet Engine Studies] PDF Online Free](https://books.google.com/books/content/images/frontcover/MT7nugEACAAJ?fife=w200-h370)
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781725989283
Total Pages : 42 pages
Book Rating : 4.9/5 (892 download)
Download or read book Internal Flow Characteristics of a Multistage Compressor with Inlet Pressure Distortion. [j85-13 Turbojet Engine Studies] written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-22 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: The measured distribution of compressor interstage pressures and temperatures resulting from a 180 deg inlet-total-pressure distortion for a J85-13 turbojet engine is reported. Extensive inner stage instrumentation combined with stepwise rotation of the inlet distortion gave data of high circumferential resolution. The steady-state pressures and temperatures along with the amplitude, extent, and location of the distorted areas are given. Data for 80, 90, and 100 percent of rotor design speed are compared with clean (undistorted) inlet flow conditions to show pressure and temperature behavior within the compressor. Both overall and stagewise compressor performances vary only slightly when clean and distorted inlet conditions are compared. Total and static pressure distortions increase in amplitude in the first few stages of the compressor and then attenuate fairly uniformly to zero at the discharge. Total-temperature distortion induced by the pressure distortion reached a maximum amplitude by the first two stages and decayed only a little through the rest of the compressor. Distortion amplitude tended to peak in line with the screen edges, and, except for total and static pressure in the tip zone, there was little swirl in the axial direction. Debogdan, C. E. and Moss, J. E., Jr. and Braithwaite, W. M. Glenn Research Center NASA-TM-X-3446, E-8848 RTOP 505-05...
Author : William H. Gauden
Publisher :
ISBN 13 :
Total Pages : 238 pages
Book Rating : 4.:/5 (785 download)
Download or read book Performance and Stalling Behavior of an Axial-flow Compressor Subjected to Three Circumferential Inlet Distortion Levels written by William H. Gauden and published by . This book was released on 1977 with total page 238 pages. Available in PDF, EPUB and Kindle. Book excerpt:
