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contributor authorH. S. Wijesinghe
contributor authorC. S. Tan
contributor authorE. E. Covert
date accessioned2017-05-09T00:09:02Z
date available2017-05-09T00:09:02Z
date copyrightApril, 2002
date issued2002
identifier issn0889-504X
identifier otherJOTUEI-28695#269_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/127646
description abstractA two-dimensional computational study was conducted to characterize the density wake induced force and moment fluctuations on a compressor blade row. The flow simulations indicate unsteady blade excitation generated by: (1) density wake fluid directed to the blade suction surface, (2) axial deflection of the blade passage shock wave position and (3) formation of a separation bubble on the blade suction surface. The blade force and moment fluctuation amplitudes are found to scale with the nondimensional density wake width w/c and a nondimensional density parameter ρ*.
publisherThe American Society of Mechanical Engineers (ASME)
titleAerodynamic Response of Turbomachinery Blade Rows to Convecting Density Wakes
typeJournal Paper
journal volume124
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1311287
journal fristpage269
journal lastpage274
identifier eissn1528-8900
keywordsDensity
keywordsForce
keywordsWakes
keywordsBlades
keywordsSuction
keywordsFluids
keywordsFlow (Dynamics)
keywordsSeparation (Technology)
keywordsShock waves
keywordsFluctuations (Physics)
keywordsCompressors AND Turbomachinery
treeJournal of Turbomachinery:;2002:;volume( 124 ):;issue: 002
contenttypeFulltext


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