Numerical investigations on the steady and unsteady leakage flow and heat transfer characteristics of rotor blade squealer tip
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-011-0474-5.pdf
Reference18 articles.
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3. Chyu, M. K., Moon, H. K., Metzger, D. E., “Heat Transfer in the Tip Region of Grooved Turbine Blades”, ASME Journal of Turbomachinery, 1989, 111(1): 131–138.
4. Bunker. R. S., Bailey, J. C., Ameri, A. A., “Heat Transfer and Flow on the First-Stage Blade Tip of a Power Generation Gas Turbine: Part I: Experimental Results”, ASME Journal of Turbomachinery, 2000, 122(2): 263–271.
5. Azad, G. S., Han, J. C., Teng, S., Boyle, R. J., “Heat Transfer and Pressure Distributions on a Gas Turbine Blade Tip”, ASME Journal of Turbomachinery, 2000, 122(3): 717–724.
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