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contributor authorJ. Fang
contributor authorH. M. Atassi
date accessioned2017-05-08T23:42:48Z
date available2017-05-08T23:42:48Z
date copyrightOctober, 1993
date issued1993
identifier issn0889-504X
identifier otherJOTUEI-28633#810_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112769
description abstractA frequency domain linearized unsteady aerodynamic analysis is presented for three-dimensional unsteady vortical flows around a cascade of loaded airfoils. The analysis fully accounts for the distortion of the impinging vortical disturbances by the mean flow. The entire unsteady flow field is calculated in response to upstream three-dimensional harmonic disturbances. Numerical results are presented for two standard cascade configurations representing turbine and compressor bladings for a reduced frequency range from 0.1 to 5. Results show that the upstream gust conditions and blade sweep strongly affect the unsteady blade response.
publisherThe American Society of Mechanical Engineers (ASME)
titleNumerical Solutions for Unsteady Subsonic Vortical Flows Around Loaded Cascades
typeJournal Paper
journal volume115
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2929319
journal fristpage810
journal lastpage816
identifier eissn1528-8900
keywordsVortex flow
keywordsBlades
keywordsCascades (Fluid dynamics)
keywordsTurbines
keywordsFlow (Dynamics)
keywordsCompressors
keywordsUnsteady flow AND Airfoils
treeJournal of Turbomachinery:;1993:;volume( 115 ):;issue: 004
contenttypeFulltext


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