Implicit numerical computation of viscous high supersonic aerodynamics for a blunt-nosed “cruiser” configuration with shock fitting using the “sublime” code
Presentation / Conference
Beg, T., Beg, O., Kuharat, S., Malysheva, L., Leonard, H., Kadir, A., …Gorla, R. Implicit numerical computation of viscous high supersonic aerodynamics for a blunt-nosed “cruiser” configuration with shock fitting using the “sublime” code. Presented at ICFM 2022: 16th International Conference on Fluid Mechanics, Helsinki, Finland
The modern thrust in proposed commercial supersonic airliners is increasingly embracing “blunt-nosed” body design. Since a key drag component in aerodynamics is skin friction (viscous drag), the nose design with reduced area will reduce the skin fric... Read More about Implicit numerical computation of viscous high supersonic aerodynamics for a blunt-nosed “cruiser” configuration with shock fitting using the “sublime” code.