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Journal Articles

Internal Cooling Near Trailing Edge of a Gas Turbine Airfoil With Cooling Airflow Through Blockages With Holes

S. C. Lau, J. Cervantes, J. C. Han, R. J. Rudolph
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2008, 130(3): 031004.
https://doi.org/10.1115/1.2775489
Published Online: May 2, 2008
...S. C. Lau; J. Cervantes; J. C. Han; R. J. Rudolph Naphthalene sublimation experiments were conducted to study heat transfer for flow through blockages with holes in an internal cooling passage near the trailing edge of a gas turbine airfoil. The cooling passage was modeled as two rectangular...
View Article titled, Internal Cooling Near Trailing Edge of a Gas Turbine Airfoil With Cooling Airflow Through <span class="search-highlight">Blockages</span> With <span class="search-highlight">Holes</span>
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Topics: Air flow, Airfoils, Cooling, Flow (Dynamics), Gas turbines, Heat, Heat transfer, Mass transfer, Reynolds number, Heat transfer coefficients