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contributor authorT. R. Camp
date accessioned2017-05-09T00:01:20Z
date available2017-05-09T00:01:20Z
date copyrightJanuary, 1999
date issued1999
identifier issn0889-504X
identifier otherJOTUEI-28668#36_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123059
description abstractMeasurements are presented of a resonant acoustic phenomenon occurring in a low-speed multistage compressor. The results show that this phenomenon shares many characteristics with acoustic resonance as measured in high-speed compressors. These similarities include a rotating pressure field, several acoustic frequencies corresponding to different circumferential modes, step changes in frequency as the flow rate is increased, and acoustic frequencies that are independent of flow coefficient, shaft speed, and the axial length of the compression system. The paper includes measurements of the helical structure of the rotating pressure field and of the variation in amplitude of the acoustic signal over a stator exit plane.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Study of Acoustic Resonance in a Low-Speed Multistage Compressor
typeJournal Paper
journal volume121
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2841232
journal fristpage36
journal lastpage43
identifier eissn1528-8900
keywordsResonance
keywordsAcoustics
keywordsCompressors
keywordsFrequency
keywordsPressure
keywordsFlow (Dynamics)
keywordsMeasurement
keywordsSignals
keywordsStators AND Compression
treeJournal of Turbomachinery:;1999:;volume( 121 ):;issue: 001
contenttypeFulltext


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