Experimental and numerical investigations of shaped hole film cooling with the influence of endwall cross flow
- 1 May 2018
- journal article
- research article
- Published by Elsevier BV in International Journal of Heat and Mass Transfer
- Vol. 120, 42-55
- https://doi.org/10.1016/j.ijheatmasstransfer.2017.11.150
Abstract
No abstract availableFunding Information
- National Natural Science Foundation of China (51476082, 51506107)
This publication has 29 references indexed in Scilit:
- Turbine endwall film cooling with combustor-turbine interface gap leakage flow: Effect of incidence angleJournal of Thermal Science, 2013
- Performance Evaluation of a Novel Film-Cooling HoleJournal of Heat Transfer, 2012
- Shape optimization of a fan-shaped hole to enhance film-cooling effectivenessInternational Journal of Heat and Mass Transfer, 2010
- Double-Jet Ejection of Cooling Air for Improved Film CoolingJournal of Turbomachinery, 2006
- Gas Turbine Film CoolingJournal of Propulsion and Power, 2006
- Fan-Shaped Hole Effects on the Aero-Thermal Performance of a Film-Cooled EndwallJournal of Turbomachinery, 2005
- The Design of an Improved Endwall Film-Cooling ConfigurationJournal of Turbomachinery, 1999
- Vortical structure in the wake of a transverse jetJournal of Fluid Mechanics, 1994
- Discrete-Jet Film Cooling: A Comparison of Computational Results With ExperimentsJournal of Turbomachinery, 1994
- Flow in Curved PipesAnnual Review of Fluid Mechanics, 1983