Heat Transfer Investigation on an Internal Cooling System of a Gas Turbine Leading Edge Model
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Publisher
Elsevier BV
Reference15 articles.
1. Evaluation of Internal Heat Transfer Coefficients for Impingement Cooled Turbine Blades;Chupp;J Aircr,1969
2. Impingement Cooling Performance in Gas Turbine Airfoils Including Effects of Leading Edge Sharpness;Metzger;ASME J Eng Power,1972
3. Heat Transfer From a Row of Impinging Jets to Concave Cylindrical Surfaces;Hrycak;Int J Heat Mass Transfer,1981
4. Local Heat Transfer in Internally Cooled Turbine Airfoil Leading Edge Regions: Part I Impingement Cooling Without Film Coolant Extraction;Metzger;ASME J Turbomach,1990
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