Coupled Aerothermal-Mechanical Analysis in Single Crystal Double Wall Transpiration Cooled Gas Turbine Blades with a Large Film Hole Density (2022)

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/10.2139/ssrn.4102556

Publication URI: http://dx.doi.org/10.2139/ssrn.4102556

Type: Journal Article/Review

Parent Publication: SSRN Electronic Journal