1-3 of 3
Keywords: leading edge
Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. June 2020, 142(6): 061005.
Paper No: TURBO-19-1083
Published Online: May 28, 2020
...Nicholas E. Holgate; Peter T. Ireland; Eduardo Romero A novel airfoil leading edge film cooling design has been investigated, and its performance over conventional alternatives quantified. In conventional designs, the region near the geometric stagnation line is typically between the two most...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Turbomach. January 2019, 141(1): 011005.
Paper No: TURBO-18-1217
Published Online: October 18, 2018
... of the effects of mainstream flow turbulence on film effectiveness have been conducted on both flat plates and vane leading edges. The film cooling holes investigated were frequently within a range of blowing ratio and surface angle parameters conducive to good surface attachment of the coolant jets...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Turbomach. March 2014, 136(3): 031019.
Paper No: TURBO-13-1083
Published Online: October 25, 2013
..., and 40,000, Ro = 0.2, 0.4, and 0.6) were numerically explored. The selected geometry (a smooth radial channel) is rather simplified compared to modern leading edge cooling cavities, which are characterized by the adoption of jet impingement cooling and film cooling holes (see Elebiary and Taslim [ 12...