Research in Engineering and Aviation

Recent Developments in Impingement Array Cooling, Including Consideration of the Separate Effects of Mach Number, Reynolds Number, Temperature Ratio, and Hole Spacing

2013

Author(s): P.M. Ligrani

“Recent Developments in Impingement Array Cooling, Including Consideration of the Separate Effects of Mach Number, Reynolds Number, Temperature Ratio, and Hole Spacing´╗┐”, Impingement Jet Cooling in Gas Turbines (Editors: R. S. Amano, B. Sunden), WIT Press, Southampton, United Kingdom, 2013.´╗┐

Abstract

None Available

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