Innovative vortex cooling concept and its application to turbine airfoil trailing edge cooling design
Author:
Affiliation:
1. Kentucky, Univ., Lexington
2. Pratt & Whitney, West Palm Beach, FL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3013
Reference10 articles.
1. The vapour pressure of naphthalene
2. Heat Transfer and Pressure Drop for Short Pin-Fin Arrays With Pin-Endwall Fillet
3. Glezer, B., Moon, H.K., and O'Connell, T., 1996, "A Novel Technique for The Internal Blade Cooling," ASME 96-GT-181.
4. A review of mass transfer measurements using naphthalene sublimation
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