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This paper presents numerical results investigating the aerodynamic and aerothermal effects of mass injection applied to hypersonic sharp leading edges, in the context of active thermal protection systems. A numerical study was carried out using Eilm
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::60e8e7131aa634b86be438af6913f59b
https://ora.ox.ac.uk/objects/uuid:774fc566-5f71-4cb8-8e7f-bc8b9c0af269
https://ora.ox.ac.uk/objects/uuid:774fc566-5f71-4cb8-8e7f-bc8b9c0af269
