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contributor authorB. Paradiso
contributor authorE. Göttlich
contributor authorO. Schennach
contributor authorR. Pecnik
contributor authorA. Marn
contributor authorJ. Woisetschläger
date accessioned2017-05-09T00:30:48Z
date available2017-05-09T00:30:48Z
date copyrightJuly, 2008
date issued2008
identifier issn0889-504X
identifier otherJOTUEI-28748#031022_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/139496
description abstractThe current paper presents the results of numerical and experimental clocking investigations performed in a high-pressure transonic turbine with a downstream vane row. The objective was a detailed analysis of shock and wake interactions in such a 1.5-stage machine while clocking the vanes. Therefore, a transient 3D Navier–Stokes calculation was done for two clocking positions, and the three-dimensional results are compared with laser-Doppler-velocimetry measurements at midspan. Additionally, the second vane was equipped with fast response pressure transducers to record the instantaneous surface pressure for 20 different clocking positions at midspan.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Effect of Vane Clocking on the Unsteady Flow Field in a One-and-a-Half Stage Transonic Turbine
typeJournal Paper
journal volume130
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2777199
journal fristpage31022
identifier eissn1528-8900
keywordsPressure
keywordsFlow (Dynamics)
keywordsWakes
keywordsShock (Mechanics)
keywordsRotors
keywordsTurbines
keywordsLaser Doppler anemometry
keywordsBlades
keywordsSuction
keywordsMeasurement
keywordsUnsteady flow
keywordsFluctuations (Physics) AND Light trucks
treeJournal of Turbomachinery:;2008:;volume( 130 ):;issue: 003
contenttypeFulltext


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