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    Film Cooling and Heat Transfer on Two Cutback Trailing Edge Models With Internal Perforated Blockages

    Source: Journal of Heat Transfer:;2008:;volume( 130 ):;issue: 001::page 12201
    Author:
    Jung-ho Choi
    ,
    Ron Rudolph
    ,
    Shantanu Mhetras
    ,
    Je-Chin Han
    ,
    Sai C. Lau
    DOI: 10.1115/1.2780174
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments to study heat transfer and film cooling on the cutback trailing edge of a turbine blade with slot ejection were performed. Heat transfer from two rows of perforated blockage inserts for lateral impingement on the coolant channel walls prior to coolant ejection into the freestream was also investigated. The internal test geometry is similar to the crossover impingement hole design used in modern gas turbine blades for trailing edge cooling. A liquid crystal technique based on hue value detection was used to measure the heat transfer coefficient on a trailing edge film-cooling model with slot ejection and an internal model with perforated blockage inserts. It was also used to determine the film effectiveness on the cutback trailing edge. For the internal model with the perforated blockage inserts, Reynolds numbers based on the hydraulic diameter of the slot and exit velocity were 5000, 10,000, 20,000, and 30,000 and corresponding coolant-to-freestream velocity ratios ranged from 0.26 to 1.83 for the external model with slot ejection, respectively. The experiments were performed for two different designs, 1 and 2, with Design 1 incorporating two different configurations with a staggered/inline slot exit arrangement and Design 2 with a staggered slot exit arrangement. Both designs utilized a 90deg flow turn into the blockage inserts as an entrance to the test section to simulate a realistic blade passage design. Results show that the internal design geometry of the trailing edge and Reynolds numbers can affect heat transfer in an internal model with perforated blockage inserts. Design 2 with a wider entrance channel and a sloped land near the ejection slots provided low heat transfer coefficients in the internal as well as external model but gave higher film-cooling effectiveness from slot ejection.
    keyword(s): Heat transfer , Cooling , Coolants , Design , Flow (Dynamics) , Reynolds number , Heat transfer coefficients AND Pressure ,
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      Film Cooling and Heat Transfer on Two Cutback Trailing Edge Models With Internal Perforated Blockages

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    http://yetl.yabesh.ir/yetl1/handle/yetl/138626
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    contributor authorJung-ho Choi
    contributor authorRon Rudolph
    contributor authorShantanu Mhetras
    contributor authorJe-Chin Han
    contributor authorSai C. Lau
    date accessioned2017-05-09T00:29:15Z
    date available2017-05-09T00:29:15Z
    date copyrightJanuary, 2008
    date issued2008
    identifier issn0022-1481
    identifier otherJHTRAO-27830#012201_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/138626
    description abstractExperiments to study heat transfer and film cooling on the cutback trailing edge of a turbine blade with slot ejection were performed. Heat transfer from two rows of perforated blockage inserts for lateral impingement on the coolant channel walls prior to coolant ejection into the freestream was also investigated. The internal test geometry is similar to the crossover impingement hole design used in modern gas turbine blades for trailing edge cooling. A liquid crystal technique based on hue value detection was used to measure the heat transfer coefficient on a trailing edge film-cooling model with slot ejection and an internal model with perforated blockage inserts. It was also used to determine the film effectiveness on the cutback trailing edge. For the internal model with the perforated blockage inserts, Reynolds numbers based on the hydraulic diameter of the slot and exit velocity were 5000, 10,000, 20,000, and 30,000 and corresponding coolant-to-freestream velocity ratios ranged from 0.26 to 1.83 for the external model with slot ejection, respectively. The experiments were performed for two different designs, 1 and 2, with Design 1 incorporating two different configurations with a staggered/inline slot exit arrangement and Design 2 with a staggered slot exit arrangement. Both designs utilized a 90deg flow turn into the blockage inserts as an entrance to the test section to simulate a realistic blade passage design. Results show that the internal design geometry of the trailing edge and Reynolds numbers can affect heat transfer in an internal model with perforated blockage inserts. Design 2 with a wider entrance channel and a sloped land near the ejection slots provided low heat transfer coefficients in the internal as well as external model but gave higher film-cooling effectiveness from slot ejection.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFilm Cooling and Heat Transfer on Two Cutback Trailing Edge Models With Internal Perforated Blockages
    typeJournal Paper
    journal volume130
    journal issue1
    journal titleJournal of Heat Transfer
    identifier doi10.1115/1.2780174
    journal fristpage12201
    identifier eissn1528-8943
    keywordsHeat transfer
    keywordsCooling
    keywordsCoolants
    keywordsDesign
    keywordsFlow (Dynamics)
    keywordsReynolds number
    keywordsHeat transfer coefficients AND Pressure
    treeJournal of Heat Transfer:;2008:;volume( 130 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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