This paper describes the thermal design processes of STRATOFLY hypersonic vehicle cooling system showing either the methodology and the supporting FEM numerical simulations. It focuses on two different regions that are both subjected to severe overheating: air-intake leading edges and the combustion chamber. Final remarks on structure survivability are presented.

Cooling system of STRATOFLY hypersonic vehicle: conceptual design, numerical analysis and verification / Scigliano, Roberto; De Simone, Valeria; Fusaro, Roberta; Ferretto, Davide; Marini, Marco; Viola, Nicole. - ELETTRONICO. - 2:(2022), pp. 931-942. (Intervento presentato al convegno 33rd Congress of the International Council of the Aeronautical Sciences tenutosi a Stockholm, SE nel 4-9/09/2022).

Cooling system of STRATOFLY hypersonic vehicle: conceptual design, numerical analysis and verification

Fusaro, Roberta;Ferretto, Davide;Viola, Nicole
2022

Abstract

This paper describes the thermal design processes of STRATOFLY hypersonic vehicle cooling system showing either the methodology and the supporting FEM numerical simulations. It focuses on two different regions that are both subjected to severe overheating: air-intake leading edges and the combustion chamber. Final remarks on structure survivability are presented.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11583/2978795