Keywords = Film cooling
Experimental Investigation of the Effect of Louver Scheme Internal Bend and Exit Shape on the Film Cooling Performance over a Flat Plate

Volume 16, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 – May 26 - 28, 2015, May 2015, Pages 1-25

O. Hassan; T. Elnady


Effect of Pressure Gradient on Film Cooling From Holes Supplemented by Anti-Vortex Holes

Volume 15, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 15 – May 28 - 30, 2013, May 2013, Pages 1-19

M. A. H. Abdel-Mohimen; T. A. Meakhail; S. S. Ayad; K. El-Shazly


Numerical Study of Film Cooling Over Flat Plate

Volume 14, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 14 – May 24 - 26, 2011, May 2011, Pages 1-16

A. S. Baher-Eneel; A. F. El-Sayed; M. H. Khobeiz