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Compressibility Effects In Circumferential Inlet Distortion In Axial Compressors
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Book Synopsis Compressibility Effects in Circumferential Inlet Distortion in Axial Compressors by : Zbigniew Krzywoblocki
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:
Book Synopsis Compressibility Effects in Circumferential Inlet Distortion in Axial Compressors by : Zbigniew Krzywoblocki
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 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Compressibility Effects in Circumferential Inlet Distortion in Axial Compressors by : Zbigniew Krzywoblocki
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 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Compressor Instability with Integral Methods by : Eddie Y.K. Ng
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.
Book Synopsis Circumferential Distortion of the Inlet Flow in an Axial Compressor by : Marvin Stanley Shinbaum
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:
Book Synopsis Unsteady Effects of Circumferential Pressure Distorted Inlet Flows in Compressors by : R. E. Peacock
Download or read book Unsteady Effects of Circumferential Pressure Distorted Inlet Flows in Compressors written by R. E. Peacock and published by . This book was released on 1981 with total page 147 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of the mechanics of rotor unsteady response in the presence of both upstream generated planar distortion and rotating stall is described. To this end, a system for the measurement and analysis of on-rotor pressure data was developed on a single stage, low speed rig. Two areas of investigation based on the compressor operating conditions were pursued: operation on the negative slope of the characteristic (nominally stable flow) and on the positive and zero slope (rotating stall). Compressor overall performance and detailed response followed trends anticipated by the blockage effects of the inlet disposed screens. Two classes of rotating stall were isolated, each with different characteristics. One was present under low flow uniform inlet conditions and the other when an inlet distortion was present. (Author).
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)
Book Synopsis Task IV by : National Aeronautics and Space Administration (NASA)
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
Book Synopsis 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 by : William H. Robbins
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:
Book Synopsis The Attenuation of Circumferential Inlet Distortion in Multi-stage Axial Compressors by : G. A. Plourde
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:
Book Synopsis Active Stabilization of Axial Compressors with Circumferential Inlet Distortion by : C. M. van Schalkwyk
Download or read book Active Stabilization of Axial Compressors with Circumferential Inlet Distortion written by C. M. van Schalkwyk and published by . This book was released on 1997 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Orlando, FL, Jun 2 - Jun 5, 1997.
Book Synopsis Performance Characteristics of an Axial-flow Compressor Operating with Circumferential Inlet Flow Distortion by : Ross Bakke Gridley
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:
Book Synopsis Circumferential Inlet Distortions in an Axial Flow Compressor by : Frank R. Carter
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:
Book Synopsis Compressibility Effects on Rotating Stall in a Two-stage Axial Compressor by : Jaideep Sahai Mathur
Download or read book Compressibility Effects on Rotating Stall in a Two-stage Axial Compressor written by Jaideep Sahai Mathur and published by . This book was released on 1987 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Circumferential Distortion of the Inlet Flow in an Axial Compressor. by : Marvin S Shinbaum
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 :North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development Publisher : ISBN 13 : Total Pages :194 pages Book Rating :4.0/5 ( download)
Book Synopsis Distortion Induced Engine Instability by : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Download or read book Distortion Induced Engine Instability written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1974 with total page 194 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Screen-induced Total-pressure Distortion on Axial-flow Compressor Stability by : James E. Calogeras
Download or read book Effect of Screen-induced Total-pressure Distortion on Axial-flow Compressor Stability written by James E. Calogeras and published by . This book was released on 1974 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Circumferential inlet flow distortions in multi-stage axial compressors by : Hans Georg Mokelke
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:
