CHT Assessment of a 3-D Vane with Cooling and Comparison to Experiments

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  • Last update: 29 December 2016
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The High Impact Technologies (HIT) Research Turbine Vane at the U.S. Air Force Research Laboratory is a three-dimensional, fully film-cooled modern turbine inlet vane.  In this paper, Captain Jamie Johnson and Paul King from the Air Force Institute of Technology conduct conjugate heat transfer analysis on the vane using Code Leo and compare the predictions to experiments.  Copyright 2011 American Institute of Aeronautics and Astronautics.  Posted with permission.