01.2 - Aircraft Design and Integrated System (Applications)
COOLING SYSTEM OF STRATOFLY HYPERSONIC VEHICLE: CONCEPTUAL DESIGN, NUMERICAL ANALYSIS AND VERIFICATION
R. Sciglianoš, V. De Simoneš, R. Fusaro˛, D. Ferretto˛, M. Mariniš, N. Viola˛; šItalian Aerospace Research Center - CIRA scpa, Italy ;˛Politecnico di Torino (PoliTo), Italy
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.