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contributor authorF. B. Metzger
contributor authorD. B. Hanson
date accessioned2017-05-09T01:36:24Z
date available2017-05-09T01:36:24Z
date copyrightJanuary, 1973
date issued1973
identifier issn1528-8919
identifier otherJETPEZ-26702#19_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163791
description abstractThe Q-FAN™, a new low pressure ratio, low noise propulsor, is currently under intensive development. Since the operating regime of the Q-FAN differs from that of the turbofan, the dominant noise sources also differ. This paper includes a summary of the results of extensive noise tests on a Q-FAN model, a discussion of the sources of various components of measured fan noise, and the results of analytical studies using a new theory to define minimum noise fan configurations.
publisherThe American Society of Mechanical Engineers (ASME)
titleLow Pressure Ratio Fan Noise Experiment and Theory
typeJournal Paper
journal volume95
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3445689
journal fristpage19
journal lastpage26
identifier eissn0742-4795
keywordsPressure
keywordsNoise (Sound) AND Turbofans
treeJournal of Engineering for Gas Turbines and Power:;1973:;volume( 095 ):;issue: 001
contenttypeFulltext


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