Momentum and thermal boundary layers on turbine airfoil suction surfaces
Author:
Affiliation:
1. Pratt and Whitney, East Hartford, CT
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-1918
Reference37 articles.
1. Convective Heat Transfer to Gas Turbine Blade Surfaces
2. Heat transfer to turbine blading in the presence of secondary flow
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