Effect of vane/blade relative position on heat transfer characteristics in a stationary turbine blade: Part 1. Tip and shroud
Author:
Publisher
Elsevier BV
Subject
General Engineering,Condensed Matter Physics
Reference40 articles.
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3. G.S. Azad, J.C. Han, S. Teng, R.J. Boyle, Heat transfer and pressure distributions on a gas turbine blade tip, ASME Paper No. 2000-GT-194, 2000
4. G.S. Azad, J.C. Han, R.J. Boyle, Heat transfer and flow on the Squealer tip of a gas turbine blade, ASME Paper No. 2000-GT-195, 2000
5. Heat transfer coefficients on the squealer tip and near squealer tip regions of a gas turbine blade;Kwak;ASME Journal of Heat Transfer,2003
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