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contributor authorKenneth W. Van Treuren
contributor authorTerrence Simon
contributor authorMarc von Koller
contributor authorAaron R. Byerley
contributor authorJames W. Baughn
contributor authorRichard Rivir
date accessioned2017-05-09T00:09:03Z
date available2017-05-09T00:09:03Z
date copyrightJanuary, 2002
date issued2002
identifier issn0889-504X
identifier otherJOTUEI-28693#100_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/127663
description abstractWith the new generation of gas turbine engines, low Reynolds number flows have become increasingly important. Designers must properly account for transition from laminar to turbulent flow and separation of the flow from the suction surface, which is strongly dependent upon transition. Of interest to industry are Reynolds numbers based upon suction surface length and flow exit velocity below 150,000 and as low as 25,000. In this paper, the extreme low end of this Reynolds number range is documented by way of pressure distributions, loss coefficients, and identification of separation zones. Reynolds numbers of 25,000 and 50,000 and with 1 percent and 8-9 percent turbulence intensity of the approach flow (free-stream turbulence intensity, FSTI) were investigated. At 25,000 Reynolds number and low FSTI, the suction surface displayed a strong and steady separation region. Raising the turbulence intensity resulted in a very unsteady separation region of nearly the same size on the suction surface. Vortex generators were added to the suction surface, but they appeared to do very little at this Reynolds number. At the higher Reynolds number of 50,000, the low-FSTI case was strongly separated on the downstream portion of the suction surface. The separation zone was eliminated when the turbulence level was increased to 8-9 percent. Vortex generators were added to the suction surface of the low-FSTI case. In this instance, the vortices were able to provide the mixing needed to re-establish flow attachment. This paper shows that massive separation at very low Reynolds numbers (25,000) is persistent, in spite of elevated FSTI and added vortices. However, at a higher Reynolds number, there is opportunity for flow reattachment either with elevated free-stream turbulence or with added vortices. This may be the first documentation of flow behavior at such low Reynolds numbers. Although it is undesirable to operate under these conditions, it is important to know what to expect and how performance may be improved if such conditions are unavoidable.
publisherThe American Society of Mechanical Engineers (ASME)
titleMeasurements in a Turbine Cascade Flow Under Ultra Low Reynolds Number Conditions
typeJournal Paper
journal volume124
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1415736
journal fristpage100
journal lastpage106
identifier eissn1528-8900
keywordsPressure
keywordsFlow (Dynamics)
keywordsSeparation (Technology)
keywordsMeasurement
keywordsSuction
keywordsReynolds number
keywordsTurbines
keywordsTurbulence
keywordsVortices
keywordsBlades AND Generators
treeJournal of Turbomachinery:;2002:;volume( 124 ):;issue: 001
contenttypeFulltext


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