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contributor authorM. Y. Jabbari
contributor authorR. J. Goldstein
date accessioned2017-05-08T23:04:44Z
date available2017-05-08T23:04:44Z
date copyrightApril, 1978
date issued1978
identifier issn1528-8919
identifier otherJETPEZ-26740#303_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/91003
description abstractResults of an experimental investigation of film cooling and heat transfer following injection through two staggered rows of holes are reported. The two staggered rows are considerably more effective in protecting the wall than a single row. The film cooling effectiveness at locations beyond about 30-hole dia downstream of injection is laterally uniform. The heat transfer coefficient is within a few percent of that without injection at low blowing rates, but it increases rapidly as the blowing rate increases above unity.
publisherThe American Society of Mechanical Engineers (ASME)
titleAdiabatic Wall Temperature and Heat Transfer Downstream of Injection Through Two Rows of Holes
typeJournal Paper
journal volume100
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3446350
journal fristpage303
journal lastpage307
identifier eissn0742-4795
keywordsHeat transfer
keywordsWall temperature
keywordsCooling AND Heat transfer coefficients
treeJournal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 002
contenttypeFulltext


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