Minimising stresses in double wall transpiration cooled components for high temperature applications (2021)

First Author: Skamniotis C
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.ijmecsci.2020.105983

Publication URI: http://dx.doi.org/10.1016/j.ijmecsci.2020.105983

Type: Journal Article/Review

Parent Publication: International Journal of Mechanical Sciences