MAXIMIZATION OF COOLING EFFECTIVENESS OF TURBINE BLADE SURFACES USING DIFFERENT ARRANGEMENT OF COOLING HOLES AND VARIOUS BLOWING RATIOS
In gas turbines, the operating temperature of the primary fluid is very high. In order to lessen the damage of turbine blades due to severe working temperature, film cooling holes are commonly implemented during designing of turbine blades. Film cooling effectiveness has been studied numerically to...
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| Principais autores: | , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
Taylor's University
2018-04-01
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| coleção: | Journal of Engineering Science and Technology |
| Assuntos: | |
| Acesso em linha: | http://jestec.taylors.edu.my/Vol%2013%20issue%204%20April%202018/13_4_6.pdf |
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