Oxidation Response of Transpiration-Cooled ZrB2 on a Hypersonic Stagnation Point (2022)

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/10.2514/1.a35309

Publication URI: http://dx.doi.org/10.2514/1.a35309

Type: Journal Article/Review

Parent Publication: Journal of Spacecraft and Rockets

Issue: 5