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Numerical investigation of vortices generator influence on the supersonic flow around wing
V. E. Borisov, T. V. Konstantinovskaya, A. E. Lutsky Keldysh Institute of Applied Mathematics RAS
Abstract:
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.
Received: 22.11.2023 Revised: 22.11.2023 Accepted: 04.12.2023
Citation:
V. E. Borisov, T. V. Konstantinovskaya, A. E. Lutsky, “Numerical investigation of vortices generator influence on the supersonic flow around wing”, Mat. Model., 36:4 (2024), 3–23; Math. Models Comput. Simul., 16:6 (2024), 791–805
Linking options:
https://www.mathnet.ru/eng/mm4549 https://www.mathnet.ru/eng/mm/v36/i4/p3
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| Abstract page: | 257 | | Full-text PDF : | 56 | | References: | 79 | | First page: | 30 |
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