Oxidation response of transpiration-cooled ZrB2 on a hypersonic stagnation point

This work presents the oxidation response of a transpiration-cooled hypersonic stagnation point made of porous ZrB2. Low-order models are used to calculate the surface temperature and oxygen concentration for a given flight condition. An analytical material oxidation model computes the surface reces...

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Bibliographic Details
Main Authors: Ewenz Rocher, M, Hermann, T, McGilvray, M
Format: Journal article
Language:English
Published: American Institute of Aeronautics and Astronautics 2022