Conjugate Heat Transfer Archive
Conjugate Heat Transfer Files
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 Tec
In this paper from Turbo Expo 2013, a conjugate heat transfer analysis of a film cooled turbine vane consisting of
A conjugate heat transfer analysis methodology is defined and applied to a film cooled turbine vane consisting of 648 cooling holes
Technical paper from the 49th AIAA Aerospace Sciences Meeting comparing the film cooled vaned simulations to experimental data.