Tool for Rapid Transient Transpiration Cooled Re-Entry Simulation - Dataset

This paper presents a numerical model intended for a system study of transpiration cooled thermal protection systems. The code PIRATE(Porous ImpulseResponse Analysis forTranspiration cooling Evaluation) enables rapid transient calculations for thermal protection systems of hypersonic flight vehicles...

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Détails bibliographiques
Auteurs principaux: Hermann, T, Naved, I, McGilvray, M
Format: Dataset
Langue:English
Publié: University of Oxford 2022