Full-Scale Turbine Vane Endwall Film-Cooling Effectiveness Distribution Using Pressure-Sensitive Paint Technique

Researchers in gas turbine field take great interest in the cooling performance on the first-stage vane because of the complex flow characteristics and intensive heat load that comes from the exit of the combustion chamber. A better understanding is needed on how the coolant flow interacts with the...

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Veröffentlicht in:	Journal of turbomachinery 2016-05, Vol.138 (5)
Hauptverfasser:	Shiau, Chao-Cheng, Chen, Andrew F, Han, Je-Chin, Azad, Salam, Lee, Ching-Pang
Format:	Artikel
Sprache:	eng
Schlagworte:	Channels Coolants Cooling Engines Pressure-sensitive paints Three dimensional Turbines Vanes
Online-Zugang:	Volltext
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