Designing against severe stresses at compound cooling holes of double wall transpiration cooled engine components (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.ast.2021.106856

Publication URI: http://dx.doi.org/10.1016/j.ast.2021.106856

Type: Journal Article/Review

Parent Publication: Aerospace Science and Technology