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contributor authorC. Camci
contributor authorT. Arts
date accessioned2017-05-08T23:34:06Z
date available2017-05-08T23:34:06Z
date copyrightJuly, 1990
date issued1990
identifier issn0889-504X
identifier otherJOTUEI-28604#497_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107740
description abstractThe present paper deals with an experimental convective heat transfer investigation around a film-cooled, high-pressure gas turbine rotor blade mounted in a stationary, linear cascade arrangement. The measurements were performed in the von Karman Institute Isentropic Light Piston Compression Tube facility. The test blade was made of Macor glass ceramic and was instrumented with thin film gages. The coolant flow was ejected simultaneously through the leading edge (three rows of holes), the suction side (two rows of holes), and the pressure side (one row of holes). The effects of overall mass weight ratio, coolant to free-stream temperature ratio, and free-stream turbulence were successively investigated.
publisherThe American Society of Mechanical Engineers (ASME)
titleAn Experimental Convective Heat Transfer Investigation Around a Film-Cooled Gas Turbine Blade
typeJournal Paper
journal volume112
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2927685
journal fristpage497
journal lastpage503
identifier eissn1528-8900
keywordsConvection
keywordsGas turbines
keywordsBlades
keywordsCoolants
keywordsCascades (Fluid dynamics)
keywordsHigh pressure (Physics)
keywordsRotors
keywordsCompression
keywordsPistons
keywordsWeight (Mass)
keywordsPressure
keywordsThin films
keywordsFlow (Dynamics)
keywordsTemperature
keywordsCeramics
keywordsGlass
keywordsMeasurement
keywordsGages
keywordsTurbulence AND Suction
treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 003
contenttypeFulltext


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