Coupled aerothermal-mechanical analysis in single crystal double wall transpiration cooled gas turbine blades with a large film hole density (2023)

First Author: Courtis M
Attributed to:  Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1016/j.applthermaleng.2022.119329

Publication URI: http://dx.doi.org/10.1016/j.applthermaleng.2022.119329

Type: Journal Article/Review

Parent Publication: Applied Thermal Engineering