Development of a Steady-State Experimental Facility for the Analysis of Double-Wall Effusion Cooling Geometries (2019)

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/10.1115/1.4041751

Publication URI: http://dx.doi.org/10.1115/1.4041751

Type: Journal Article/Review

Parent Publication: Journal of Turbomachinery

Issue: 4

ISSN: 15288900 0889504X