Zobrazeno 1 - 10
of 42
pro vyhledávání: '"Meiliang, Mao"'
Publikováno v:
Entropy, Vol 26, Iss 4, p 334 (2024)
Based on a 5-point stencil and three 3-point stencils, a nonlinear multi-order weighted method adaptive to 5-3-3-3 stencils for shock capturing is presented in this paper. The form of the weighting function is the same as JS (Jiang–Shu) weighting;
Externí odkaz:
https://doaj.org/article/0a02bfcf440e4601af35360c475957df
Publikováno v:
AIP Conference Proceedings; 2024, Vol. 2996 Issue 1, p1-10, 10p
Publikováno v:
Advances in Aerodynamics, Vol 1, Iss 1, Pp 1-24 (2019)
Abstract This paper presents an engineering-oriented UGKS solver package developed in China Aerodynamics Research and Development Center (CARDC). The solver is programmed in Fortran language and uses structured body-fitted mesh, aiming for predicting
Externí odkaz:
https://doaj.org/article/21f06c2461da43979597913fe6335485
Publikováno v:
Entropy, Vol 24, Iss 6, p 836 (2022)
Strong viscous interaction and multiple flow regimes exist when vehicles fly at high altitude and high Mach number conditions. The Navier–Stokes(NS) solver is no longer applicable in the above situation. Instead, the direct simulation Monte Carlo (
Externí odkaz:
https://doaj.org/article/6bb3ecf6bc9f455aab4ab1ed58bb4766
Publikováno v:
Advances in Applied Mathematics and Mechanics. 14:415-441
Publikováno v:
2022 6th High Performance Computing and Cluster Technologies Conference (HPCCT).
Publikováno v:
2022 6th High Performance Computing and Cluster Technologies Conference (HPCCT).
Publikováno v:
Advances in Aerodynamics, Vol 1, Iss 1, Pp 1-24 (2019)
This paper presents an engineering-oriented UGKS solver package developed in China Aerodynamics Research and Development Center (CARDC). The solver is programmed in Fortran language and uses structured body-fitted mesh, aiming for predicting aerodyna
Publikováno v:
31ST INTERNATIONAL SYMPOSIUM ON RAREFIED GAS DYNAMICS: RGD31.
The interaction flow fields between a continuum jet and the hypersonic free stream with altitudes ranging between 70 and 100 km are simulated with a two-dimensional implicit Unified Gas Kinetic Scheme (UGKS) solver. It is shown that the boundary laye
Publikováno v:
Advances in Applied Mathematics and Mechanics. 8:670-692
We compare in this paper the properties of Osher flux with O-variant and P-variant (Osher-O flux and Osher-P flux) in finite volume methods for the two-dimensional Euler equations and propose an entropy fix technique to improve their robustness. We c