Author:
Bacci Tommaso,Gamannossi Andrea,Mazzei Lorenzo,Picchi Alessio,Winchler Lorenzo,Carcasci Carlo,Andreini Antonio,Abba Luca,Vagnoli Stefano
Reference13 articles.
1. Ho K.S., Liu J.S., Elliott T. and Aguilar B. “Conjugate heat transfer analysis for gas turbine film-cooled blade” ASME Paper GT2016-56688, (2016).
2. Hylton L. D., Mihelc M. S., Turner E. R., Nealy D. A. and York R. E. “Analytical and experimental evaluation of the heat transfer distribution over the surfaces of turbine vanes.” NASA Contractor Report, NASA CR-168015, (1983).
3. Gas TurbineHeat Transferand Cooling Technology;Han,2013
4. A transient infrared thermographymethod for simultaneous film effectiveness and heat transfer coefficient measurementsfrom a single test.;Ekkad;Journal of Turbomachinery,2004
5. Lynch S. and Thole K. “The effect of combustor-turbine interface gap leakage on the endwall heat transfer for a nozzle guide vane.” ASME Paper.
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