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Film Cooled Turbine Blade Analysis

	Posted Mon July 15, 2013 @10:56AM
	Please join Aerodynamic Solutions on July 23rd from 11am - 12pm EST as the ADS team led by Chairman and CTO Bob Ni presents a comparison between the predictions from conjugate heat transfer analysis of a 648 hole film cooled turbine vane to experimental data.

	The conjugate heat transfer analysis capability used in this study was developed under an SBIR Phase II grant from the U.S. Air Force and has been integrated into the ADS Master Edition. Sign up here.

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