A Numerical Investigation of Heat Transfer Characteristics with Varying Film Cooling Hole Shapes for Gas Turbine Blade Cooling
Recently, film cooling has been continuously studied to increase the efficiency of gas turbines. A turbine inlet temperature increase occurs as a way to improve the efficiency. However, it is essential to improve the cooling performance of the blade surface because of the melting point of the part....
محفوظ في:
| المؤلفون الرئيسيون: | , , , , |
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| التنسيق: | Artigo |
| اللغة: | Inglês |
| منشور في: |
Korean Society for Precision Engineering
2022-06-01
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| سلاسل: | 한국정밀공학회지 |
| الموضوعات: | |
| الوصول للمادة أونلاين: | http://www.jkspe.or.kr/upload/pdf/NODE11067907.pdf |
| الوسوم: |
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