Effects of rim location, rim height, and tip clearance on the tip and near tip region heat transfer of a gas turbine blade
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference34 articles.
1. R.E. Mayle, D.E. Metzger, Heat transfer at the tip of an unshrouded turbine blade, in: Proc. Seventh Int. Heat Transfer Conf., Hemisphere Pub, 1982, pp. 87–92
2. The influence of turbine clearance gap leakage on passage velocity and heat transfer near blade tips. Part I: sink flow effects on blade pressure side;Metzger;ASME J. Turbomach.,1989
3. The influence of turbine clearance gap leakage on passage velocity and heat transfer near blade tips. Part II: source flow effects on blade pressure side;Rued;ASME J. Turbomach.,1989
4. Cavity heat transfer on a transverse grooved wall in a narrow flow channel;Metzger;J. Heat Transfer,1989
5. Heat transfer in the tip region of grooved turbine blades;Chyu;J. Turbomach.,1989
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