Numerical investigation of vortices generator influence on the supersonic flow around wing
Matematičeskoe modelirovanie, Tome 36 (2024) no. 4, pp. 3-23

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The paper presents the results of a numerical investigation and analysis of the effect of vortex structures from an upstream generator wing on the supersonic flow around the main wing. Effect of the generator wing span is also considered. Numerical results were obtained on the multiprocessor hybrid supercomputer system K-60 at the Keldysh Institute of Applied Mathematics RAS.
Keywords: wing tandem, supersonic flow, supersonic vortices interaction, influence of incoming flow disturbances.
@article{MM_2024_36_4_a0,
     author = {V. E. Borisov and T. V. Konstantinovskaya and A. E. Lutsky},
     title = {Numerical investigation of vortices generator influence on the supersonic flow around wing},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {3--23},
     publisher = {mathdoc},
     volume = {36},
     number = {4},
     year = {2024},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2024_36_4_a0/}
}
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V. E. Borisov; T. V. Konstantinovskaya; A. E. Lutsky. Numerical investigation of vortices generator influence on the supersonic flow around wing. Matematičeskoe modelirovanie, Tome 36 (2024) no. 4, pp. 3-23. http://geodesic.mathdoc.fr/item/MM_2024_36_4_a0/