Tool for rapid transient transpiration cooled re-entry simulation

Tool for rapid transient transpiration cooled re-entry simulation

This Paper presents a numerical model intended for a system study of transpiration-cooled thermal protection systems. The code PIRATE enables rapid transient calculations for thermal protection systems of hypersonic flight vehicles. In the code, semi-empirical aerodynamic correlations are employed....

Полное описание

Библиографические подробности
Главные авторы:	Hermann, T, Naved, I, McGilvray, M
Формат:	Journal article
Опубликовано:	American Institute of Aeronautics and Astronautics 2019

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