An Experimental and Numerical Study of Heat Transfer and Pressure Loss in a Rectangular Channel With V-Shaped Ribs
Author:
Affiliation:
1. Institute of Aerospace Thermodynamics, University of Stuttgart, Stuttgart, D-70569 Germany
2. ALSTOM (Switzerland) Ltd., Technology Center TTC-TT, Birr, CH-5242 Switzerland
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/129/4/800/5844432/800_1.pdf
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3. Bailey, J. C., Tolpadi, A. K., Intile, J., Fric, T. F., Nirmalan, N. V., and Bunker, R. S., 2002, “Experimental and Numerical Study of Heat Transfer in a Gas Turbine Combustor Liner,” ASME Paper No. GT2002-30183.
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5. Cakan, M. , 2000, “Aero-Thermal Performance of Internal Cooling Systems in Turbo Machines,” Lecture Series 2000–03, von Karman Institute for Fluid Dynamics.
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