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Calculation of high-speed flows based on a hyperbolic quasi-gas dynamic system
A. E. Lutsky, A. V. Severin, Ya. V. Khankhasaeva Keldysh Institute of Applied Mathematics RAS
Abstract:
Numerical algorithm for unstructured grids based on the compact version of hyperbolic
system of quasi-gas-dynamic equations was developed and implemented on modern multiprocessor computing systems K-100 and K-60 (Keldysh Institute of Applied Mathematics RAS). Simulations of the flow around a high speed aircraft model was carried out for
Mach number M=6 and various angles of attack. Numerical simulation of unsteady flow
in the air intake channel was made.
Keywords:
quasi-gas-dynamic system of equations, supersonic flow, unsteady flow in the air intake channel.
Received: 02.11.2021 Revised: 02.12.2021 Accepted: 06.12.2021
Citation:
A. E. Lutsky, A. V. Severin, Ya. V. Khankhasaeva, “Calculation of high-speed flows based on a hyperbolic quasi-gas dynamic system”, Matem. Mod., 34:2 (2022), 17–31; Math. Models Comput. Simul., 14:5 (2022), 700–709
Linking options:
https://www.mathnet.ru/eng/mm4351 https://www.mathnet.ru/eng/mm/v34/i2/p17
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Abstract page: | 215 | Full-text PDF : | 60 | References: | 42 | First page: | 6 |
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