21st AIAA Advanced Measurement and Ground Testing Technology Conference: 00-2201 - 00-2374
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Page : 522 pages
File Size : 17,30 MB
Release : 2000
Category : Aerodynamics
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Page : 522 pages
File Size : 17,30 MB
Release : 2000
Category : Aerodynamics
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Page : 714 pages
File Size : 38,74 MB
Release : 1999
Category : Aeronautics
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Page : 594 pages
File Size : 39,21 MB
Release : 2002
Category : Aircraft gas-turbines
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Page : 18 pages
File Size : 12,72 MB
Release : 1999
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Page : 16 pages
File Size : 44,20 MB
Release : 2001
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Page : 1016 pages
File Size : 46,79 MB
Release : 1999
Category : Aeronautics
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Page : 20 pages
File Size : 12,48 MB
Release : 2000
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Page : 376 pages
File Size : 38,94 MB
Release : 2001
Category : Optical fiber detectors
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Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 28 pages
File Size : 27,13 MB
Release : 2018-05-29
Category :
ISBN : 9781720381679
Compressor stall is a catastrophic breakdown of the flow in a compressor, which can lead to a loss of engine power, large pressure transients in the inlet/nacelle and engine flameout. The implementation of active or passive strategies for controlling rotating stall and surge can significantly extend the stable operating range of a compressor without substantially sacrificing performance. It is crucial to identify the dynamic changes occurring in the flow field prior to rotating stall and surge in order to successfully control these events. Generally, pressure transducer measurements are made to capture the transient response of a compressor prior to rotating stall. In this investigation, Digital Particle Imaging Velocimetry (DPIV) is used in conjunction with dynamic pressure transducers to simultaneously capture transient velocity and pressure measurements in the non-stationary flow field during compressor surge. DPIV is an instantaneous, planar measurement technique which is ideally suited for studying transient flow phenomena in high speed turbomachinery and has been used previously to successfully map the stable operating point flow field in the diffuser of a high speed centrifugal compressor. Through the acquisition of both DPIV images and transient pressure data, the time evolution of the unsteady flow during surge is revealed.Wernet, Mark P. and Bright, Michelle M. and Skoch, Gary J.Glenn Research CenterCENTRIFUGAL COMPRESSORS; ROTATING STALLS; PARTICLE IMAGE VELOCIMETRY; PRESSURE MEASUREMENT; DYNAMIC PRESSURE; PRESSURE SENSORS; TRANSIENT PRESSURES; UNSTEADY FLOW
Author : Sushabhan Choudhury
Publisher : Springer Nature
Page : 966 pages
File Size : 13,93 MB
Release : 2019-08-28
Category : Technology & Engineering
ISBN : 9811386188
The book focuses on the integration of intelligent communication systems, control systems, and devices related to all aspects of engineering and sciences. It includes high-quality research papers from the 3rd international conference, ICICCD 2018, organized by the Department of Electronics, Instrumentation and Control Engineering at the University of Petroleum and Energy Studies, Dehradun on 21–22 December 2018. Covering a range of recent advances in intelligent communication, intelligent control and intelligent devices., the book presents original research and findings as well as researchers’ and industrial practitioners’ practical development experiences of.