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contributor authorA. N. Abdelhamid
date accessioned2017-05-09T00:56:08Z
date available2017-05-09T00:56:08Z
date copyrightOctober, 1971
date issued1971
identifier issn1528-8919
identifier otherJETPEZ-26696#431_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/150834
description abstractDiscrete frequency noise characteristics of a research lifting fan is investigated analytically. Based on steady aerodynamic data of the fan, unsteady aerodynamic forces acting on the rotor and stator blades were calculated using the results of previous investigators and an analysis which determines the effect of fluctuating velocity disturbance parallel to blade chord on the unsteady lift of cambered thin airfoils. The calculated unsteady forces were then used to determine the characteristics of discrete frequency noise emission from the fan. For the fan under consideration it is shown that the rotor interaction noise dominates the fan noise. Comparison between the predicted sound pressure levels and experimental observations shows good agreement. Based on the calculated detailed contributions of the different force harmonics acting on the blades to the fan noise, possible means of reducing lifting fan noise are discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleDiscrete Frequency Noise From Lifting Fans
typeJournal Paper
journal volume93
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3445603
journal fristpage431
journal lastpage440
identifier eissn0742-4795
keywordsNoise (Sound)
keywordsFans
keywordsBlades
keywordsForce
keywordsRotors
keywordsAerodynamics
keywordsSound pressure
keywordsChords (Trusses)
keywordsStators
keywordsEmissions AND Airfoils
treeJournal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 004
contenttypeFulltext


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