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contributor authorM. T. Schobeiri
contributor authorB. Öztürk
date accessioned2017-05-09T00:14:40Z
date available2017-05-09T00:14:40Z
date copyrightOctober, 2004
date issued2004
identifier issn0889-504X
identifier otherJOTUEI-28715#663_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130969
description abstractThe paper experimentally studies the effects of periodic unsteady wake flow on boundary layer development, separation and reattachment along the suction surface of a low pressure turbine blade. The experimental investigations were performed on a large scale, subsonic unsteady turbine cascade research facility at the Turbomachinery Performance and Flow Research Laboratory (TPFL), Texas A&M University. The experiments were carried out at a Reynolds number of 110,000 (based on suction surface length and exit velocity) with a free-stream turbulence intensity of 1.9%. One steady and two different unsteady inlet flow conditions with the corresponding passing frequencies, wake velocities, and turbulence intensities were investigated. The reduced frequencies cover the entire operating range of LP turbines. In addition to the unsteady boundary layer measurements, blade surface measurements were performed at the same Reynolds number. The surface pressure measurements were also carried out at one steady and two periodic unsteady inlet flow conditions. The results presented in ensemble-averaged, and the contour plot forms help to understand the physics of the separation phenomenon under periodic unsteady wake flow. It was found that the suction surface displayed a strong separation bubble for these three different reduced frequencies. For each condition, the locations and the heights defining the separation bubble were determined by carefully analyzing and examining the pressure and the mean velocity profile data. The location of boundary layer separation was independent of the reduced frequency level. However, the extent of the separation was strongly dependent on the reduced frequency level. Once the unsteady wake started to penetrate into the separation bubble, the turbulent spot produced in the wake paths caused a reduction of the separation bubble height.
publisherThe American Society of Mechanical Engineers (ASME)
titleExperimental Study of the Effect of Periodic Unsteady Wake Flow on Boundary Layer Development, Separation, and Reattachment Along the Surface of a Low Pressure Turbine Blade
typeJournal Paper
journal volume126
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1791646
journal fristpage663
journal lastpage676
identifier eissn1528-8900
keywordsPressure
keywordsFlow (Dynamics)
keywordsSeparation (Technology)
keywordsTurbulence
keywordsSuction
keywordsWakes
keywordsBubbles
keywordsBoundary layers
keywordsBlades
keywordsTurbine blades
keywordsCascades (Fluid dynamics)
keywordsFrequency
keywordsReynolds number
keywordsTurbines AND Measurement
treeJournal of Turbomachinery:;2004:;volume( 126 ):;issue: 004
contenttypeFulltext


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