Comparison of Heat Transfer Augmentation Techniques
Author:
Affiliation:
1. University of Utah, Salt Lake City, Utah 84112-9208
2. Pratt and Whitney Canada, United Technologies Corporation, Longueuil, Quebec J4G 1A1, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1964
Reference125 articles.
1. 2Han, J. C., Dutta, S., and Ekkad, S., Gas Turbine Heat Transfer and Cooling Technology, Taylor and Francis, New York, 2000, pp.6, 7, 251-254.
2. Length to Diameter Ratio and Row Number Effects in Short Pin Fin Heat Transfer
3. Variable Property Nusselt Numbers in a Channel with Pin Fins
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