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contributor authorDara W. Childs
contributor authorBassem Kheireddin
contributor authorStephen Phillips
contributor authorThanesh Deva Asirvatham
date accessioned2017-05-09T00:43:31Z
date available2017-05-09T00:43:31Z
date copyrightSeptember, 2011
date issued2011
identifier issn1528-8919
identifier otherJETPEZ-27172#092504_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/145950
description abstractA flat-plate tester was used to measure the friction factor behavior for a hole-pattern roughened surface apposed to a smooth surface. The tests were executed to characterize the friction factor behavior of annular seals that use a roughened-surface stator and a smooth rotor. Friction factors were obtained from measurements of the mass flow rate and static pressure measurements along the smooth and roughened surfaces. In addition, dynamic pressure measurements were made at four axial locations at the bottom of individual holes and at facing locations in the smooth plate. The test facility is described, and a procedure for determining the friction factor is reviewed. Three clearances were investigated: 0.635 mm, 0.381 mm, and 0.254 mm. Tests were conducted with air at three different inlet pressures (84 bars, 70 bars, and 55 bars), producing a Reynolds numbers range from 50,000 to 700,000. Three surface configurations were tested, including smooth-on-smooth, smooth-on-hole, and hole-on-hole. The hole-pattern plates are identical with the exception of the hole depth. For the smooth-on-smooth and smooth-on-hole configurations, the friction factor remains largely constant or increases slightly with increasing Reynolds numbers. The friction factor increases as the clearance between the plates increases. The test program was initiated to investigate a friction-factor jump phenomenon cited by (1992, “Friction-Factor Characteristics for Narrow-Channels With Honeycomb Surfaces,” Trans. ASME, J. Tribol., 114, pp. 714–721) in test results from a flat-plate tester where, at elevated values of Reynolds numbers, the friction factor began to increase steadily with increasing Reynolds numbers. They tested apposed honeycomb surfaces. For the present tests, the phenomenon was also observed for tests of apposed roughened surfaces but was not observed for smooth-on-smooth or smooth-on-rough configurations. When the phenomenon was observed, dynamic pressure measurements showed a peak-pressure oscillation at the calculated Helmholtz frequency of the holes.
publisherThe American Society of Mechanical Engineers (ASME)
titleFriction Factor Behavior From Flat-Plate Tests of Smooth and Hole-Pattern Roughened Surfaces With Supply Pressures up to 84 bars
typeJournal Paper
journal volume133
journal issue9
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4002882
journal fristpage92504
identifier eissn0742-4795
keywordsPressure
keywordsFlow (Dynamics)
keywordsFriction
keywordsClearances (Engineering)
keywordsPlates (structures)
keywordsFlat plates AND Manufacturing
treeJournal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 009
contenttypeFulltext


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