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contributor authorD. R. Poling
contributor authorD. P. Telionis
date accessioned2017-05-08T23:24:58Z
date available2017-05-08T23:24:58Z
date copyrightDecember, 1987
date issued1987
identifier issn0098-2202
identifier otherJFEGA4-27030#410_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/102571
description abstractTrailing edge flows are visualized for a pitching airfoil. The validity of the quasi-steady and an extension to an unsteady Kutta condition, namely the Giesing-Maskell condition are examined. A new dynamic similarity parameter is proposed. Earlier work and the present results are re-evaluated in terms of this parameter. A range is identified in which no Kutta-type condition may apply.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Trailing Edge of a Pitching Airfoil at High Reduced Frequencies
typeJournal Paper
journal volume109
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3242681
journal fristpage410
journal lastpage414
identifier eissn1528-901X
keywordsFrequency
keywordsAirfoils AND Flow (Dynamics)
treeJournal of Fluids Engineering:;1987:;volume( 109 ):;issue: 004
contenttypeFulltext


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