Heat Transfer and Pressure Drop Measurements in a Rib Roughened Leading Edge Cooling Channel
Author:
Affiliation:
1. Institut für Thermodynamik der Luftund Raumfahrt, Universität Stuttgart, Pfaffenwaldring 31, D-70569 Stuttgart, Germany
2. Heat Transfer and Combustion, MTU Aero Engines GmbH, D-80995 Munich, Germany
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4004747/5850075/061006_1.pdf
Reference31 articles.
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4. Heat Transfer Technology for Internal Passages of Air-Cooled Blades for Heavy-Duty Gas Turbines;Weigand;Ann. N. Y. Acad. Sci.
5. Bunker, R., and Osgood, S., 2003, “The Effect of Turbulator Lean on Heat Transfer and Friction in a Square Channel,” Proc. ASME Turbo Expo 2003, GT2003-38137.
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