An Integrated Conjugate Computational Approach for Evaluating the Aerothermal and Thermomechanical Performance of Double-Wall Effusion Cooled Systems (2017)

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/gt2017-64711

Publication URI: http://dx.doi.org/10.1115/gt2017-64711

Type: Conference/Paper/Proceeding/Abstract