Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Dingwu Jiang"'
Autor:
Weiming Gao, Dingwu Jiang, Yiming Zhang, Yao Li, Zhilong Xu, Runxi Han, Hao Tian, Hufei Dai, Qijing Lu, Cuiping Li
Publikováno v:
ACS Omega, Vol 9, Iss 10, Pp 11431-11442 (2024)
Externí odkaz:
https://doaj.org/article/f591b1bbf1794eef9226f5f78b1aa10a
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:
Advances in Aerodynamics, Vol 3, Iss 1, Pp 1-10 (2021)
Abstract A scaled model of the X38-like configuration was simulated under hypersonic conditions for the direct simulation Monte Carlo method and the unified gas kinetic scheme. The inflow conditions considered several flow regimes, from the near-cont
Externí odkaz:
https://doaj.org/article/746672b48a944f7e96225dfe211dd2f1
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 The Navier–Stokes(NS) solver is no longer applicable in the above situation.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:
AIP Conference Proceedings; 2024, Vol. 2996 Issue 1, p1-10, 10p
Publikováno v:
2022 6th High Performance Computing and Cluster Technologies Conference (HPCCT).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d5fce35393f12904b7b430bdc90df56c
https://doi.org/10.1145/3560442.3560443
https://doi.org/10.1145/3560442.3560443
Publikováno v:
2022 6th High Performance Computing and Cluster Technologies Conference (HPCCT).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::143a0fe0842ad7f0f5147d8310426e8b
https://doi.org/10.1145/3560442.3560444
https://doi.org/10.1145/3560442.3560444
Publikováno v:
2022 6th High Performance Computing and Cluster Technologies Conference (HPCCT).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fd8bc9fcb5e6418e125439ca8a175b1d
https://doi.org/10.1145/3560442.3560446
https://doi.org/10.1145/3560442.3560446
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
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e9629f8930d6634d98cbadfd788a46ea
http://link.springer.com/article/10.1186/s42774-019-0008-5
http://link.springer.com/article/10.1186/s42774-019-0008-5