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