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contributor authorS. Gilham
contributor authorP. C. Ivey
contributor authorJ. M. Owen
date accessioned2017-05-08T23:38:26Z
date available2017-05-08T23:38:26Z
date copyrightApril, 1992
date issued1992
identifier issn1528-8919
identifier otherJETPEZ-26699#268_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/110236
description abstractSelf-induced flow occurs when a tube, open at one end and sealed at the other, is rotated about its central axis: Fluid flows along the axis from the open end toward the sealed end and returns in a layer adjacent to the inner surface of the tube. This mechanism, which can occur under isothermal or nonisothermal conditions, is believed to be responsible for the so-called “hot-poker effect” that was observed during anti-icing tests on the nose bullet of an aeroengine. This paper describes a combined theoretical and experimental study of self-induced flow. It is shown that, for the length-to-diameter (L/D) ratios and rotational Reynolds numbers associated with the anti-icing tubes of aeroengines, the laminar flow near the sealed end of the tube is similar to that of the so-called free disk. Swirl in the air outside the open end reduces the self-induced flow, but flow can reach the sealed end of a stepped tube that has either a sudden contraction or a sudden enlargement.
publisherThe American Society of Mechanical Engineers (ASME)
titleSelf-Induced Flow in a Stepped Rotating Tube
typeJournal Paper
journal volume114
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2906583
journal fristpage268
journal lastpage274
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsLaminar flow
keywordsReynolds number
keywordsDisks
keywordsBullets
keywordsMechanisms AND Fluid dynamics
treeJournal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002
contenttypeFulltext


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