Testing a Transpiration Cooled Zirconium-Di-Boride sample in the Plasma Tunnel at IRS (2019)

First Author: Ewenz Rocher M
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/10.2514/6.2019-1552

Publication URI: http://dx.doi.org/10.2514/6.2019-1552

Type: Conference/Paper/Proceeding/Abstract