An Experimentally Validated Low-Order Model of the Thermal Response of Double-Wall Effusion Cooling Systems for High-Pressure Turbine Blades (2021)

First Author: Murray A
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/10.1115/1.4050976

Publication URI: http://dx.doi.org/10.1115/1.4050976

Type: Journal Article/Review

Parent Publication: Journal of Turbomachinery

Issue: 11

ISSN: 15288900 0889504X