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contributor authorT. J. Landsberg
contributor authorE. Krasnoff
date accessioned2017-05-09T01:34:57Z
date available2017-05-09T01:34:57Z
date copyrightMarch, 1972
date issued1972
identifier issn0098-2202
identifier otherJFEGA4-27389#97_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162978
description abstractThe performance of two-dimensional jet-flap cascades is determined experimentally. Stream deflection angles are presented as a function of the ratio of jet to mainstream momentum flux at chord spacing ratios of 0.375 and 0.75. Results obtained with conventional jet-flap airfoils (normal blowing near trailing edge) are in good agreement with published theoretical results. Tangential blowing jet-flap airfoils (tangential blowing over a rounded trailing edge) are shown to approximately double the turning effectiveness of the cascade.
publisherThe American Society of Mechanical Engineers (ASME)
titleAn Experimental Study of Rectilinear Jet-Flap Cascades
typeJournal Paper
journal volume94
journal issue1
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3425399
journal fristpage97
journal lastpage104
identifier eissn1528-901X
keywordsMomentum
keywordsCascades (Fluid dynamics)
keywordsChords (Trusses)
keywordsDeflection AND Airfoils
treeJournal of Fluids Engineering:;1972:;volume( 094 ):;issue: 001
contenttypeFulltext


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