Numerical simulation on the effect of jet nozzle position on impingement cooling of gas turbine blade leading edge
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference36 articles.
1. Gas Turbine Heat Transfer and Cooling Technology;Han,2000
2. Evaluation of internal heat transfer coefficients for impingement cooled turbine airfoils;Chupp;J. Aircraft,1969
3. Impingement cooling of concave surface with lines of circular air jets;Metzger;ASME J. Eng. Power,1969
4. Impingement cooling performance in gas turbine airfoils including effects of leading edge sharpness;Metzger;ASME J. Eng. Power,1972
5. Effects of crossflow on impingement heat transfer;Metzger;ASME J. Eng. Power,1972
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