Experimental and simulation study on the effect of geometrical and flow parameters for combined-hole film cooling
Film cooling method was applied to the turbine blades to provide thermal protection from high turbine inlet temperatures in modern gas turbines. Recent literature discovers that combining two cylindrical holes of film cooling is one of the ways to further enhance the film cooling performances....
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| 格式: | Thesis |
| 语言: | English English English |
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2016
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| 在线阅读: | http://eprints.uthm.edu.my/751/1/24p%20HASWIRA%20HASSAN.pdf http://eprints.uthm.edu.my/751/2/HASWIRA%20HASSAN%20COPYRIGHT%20DECLARATION.pdf http://eprints.uthm.edu.my/751/3/HASWIRA%20HASSAN%20WATERMARK.pdf |
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