Application of the Nesvetay code for solving three-dimensional high-altitude aerodynamics problems. (English. Russian original) Zbl 1479.76066
Comput. Math. Math. Phys. 60, No. 4, 737-748 (2020); translation from Zh. Vychisl. Mat. Mat. Fiz. 60, No. 4, 752-764 (2020).
Summary: A survey of the capabilities of the Nesvetay code as applied to computing the flow of a high-speed monatomic gas around objects of irregular shape for large flight altitudes is given. An implicit numerical method on an arbitrary unstructured grid and a two-level approach to the organization of parallel computations are described. This code is compared with the well-known MONACO and SMILE codes that implement the direct simulation Monte Carlo method.
MSC:
| 76M12 | Finite volume methods applied to problems in fluid mechanics |
| 76P05 | Rarefied gas flows, Boltzmann equation in fluid mechanics |
| 76N15 | Gas dynamics (general theory) |
| 65Y05 | Parallel numerical computation |
Keywords:
kinetic equation; S-model; rarefied monatomic gas; unstructured mesh; two-level parallel supercomputer computationReferences:
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