Conjugate Heat Transfer Archive

Conjugate Heat Transfer Files

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

Updated on 29 December 2016

  • 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

Comparison of Predictions from CHT Analysis to Experimental Data

Updated on 29 December 2016

  • In this paper from Turbo Expo 2013, a conjugate heat transfer analysis of a film cooled turbine vane consisting of

Conjugate Heat Transfer Analysis of a Film Cooled Turbine Vane

Updated on 29 December 2016

  • A conjugate heat transfer analysis methodology is defined and applied to a film cooled turbine vane consisting of 648 cooling holes

Film Cooled Vane Case Study

Updated on 29 December 2016

  • Technical paper from the 49th AIAA Aerospace Sciences Meeting comparing the film cooled vaned simulations to experimental data.