Научная визуализация, 2025, том 17, номер 4, страницы 1 - 8, DOI: 10.26583/sv.17.4.01
Visual Processing of the Results of Supersonic Flow Around a Delta Wing
Авторы: Т.В. Константиновская1, В.Е. Борисов2, A.E. Луцкий3
Институт прикладной математики им. М.В. Келдыша Российской академии наук
1 ORCID: 0000-0002-1127-503X, konstantinovskaya@kiam.ru
2 ORCID: 0000-0003-4448-7474, borisov@keldysh.ru
3 ORCID: 0000-0002-4442-0571, allutsky@yandex.ru
Аннотация
The paper considers the problem of visual processing of the numerical simulation results of vortex structures in supersonic flow around delta wing. The methods of visual processing of the obtained structures using various methods of scientific identification of vortex structures and visualization of vortex flows are shown. The obtained results are compared for different incoming flow Mach numbers. The delta wing under consideration had an attack angle of 14°. Numerical simulations were performed on the hybrid supercomputer system K-60 at the Supercomputer Centre of Collective Usage of KIAM RAS.
Ключевые слова: Flow around delta wing, vortex, vortex structures identification, scientific visualization.
