Vortex structures investigation in flow around delta wing

V. E. Borisov, T. V. Konstantinovskaya, A. E. Lutsky


Abstract: The vortex structures formed behind a triangular wing during a supersonic flow around it are considered. The dependence of these structures on the angle of attack and on the incoming flow Mach number is investigated. Numerical data were obtained on the multiprocessor hybrid supercomputer system K-60 at the KIAM of the Russian Academy of Sciences.

Keywords: supersonic flow, delta wing, tip vortex.

DOI: 10.20948/prepr-2024-78