
Effects of the Condition of the Approach Boundary Layer and of Mainstream Pressure Gradients on the Heat Transfer Coefficient on Film-Cooled Surfaces
Hay, N., Lampard, D., Saluja, C. L.Volume:
107
Année:
1985
Langue:
english
Journal:
Journal of Engineering for Gas Turbines and Power
DOI:
10.1115/1.3239703
Fichier:
PDF, 587 KB
english, 1985