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2D and 3D thermoelastic phenomena in double wall transpiration cooling systems for gas turbine blades and hypersonic flight (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.2021.106610

Publication URI: http://dx.doi.org/10.1016/j.ast.2021.106610

Type: Journal Article/Review

Parent Publication: Aerospace Science and Technology