Measurement of heat transfer coefficient distributions and flow field in a model of a turbine blade cooling passage with tangential injection
In certain regions of turbine aerofoils, cooling system designers need to cool the blades with convection systems that provide high heat transfer coefficients. The present research has investigated a circular cooling passage with tangential injection suitable for a blade leading edge. The heat trans...
Главные авторы: | Ling, J, Ireland, P, Harvey, N, ASME |
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Формат: | Journal article |
Язык: | English |
Опубликовано: |
2006
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