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...

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Những tác giả chính: Ling, J, Ireland, P, Harvey, N, ASME
Định dạng: Journal article
Ngôn ngữ:English
Được phát hành: 2006