A comparative study of the film cooling hole configuration effects on the leading edge of asymmetrical turbine blade

Author: Benabed Mustapha  

Publisher: Edp Sciences

E-ISSN: 1765-2960|12|1|25-36

ISSN: 1296-2139

Source: Mécanique et Industries, Vol.12, Iss.1, 2011-04, pp. : 25-36

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Abstract