TY - JOUR
T1 - Seventh and ninth orders characteristic-wise alternative WENO finite difference schemes for hyperbolic conservation laws
AU - Gao, Zhen
AU - Fang, Li Li
AU - Wang, Bao Shan
AU - Wang, Yinghua
AU - Don, Wai Sun
N1 - Publisher Copyright:
© 2020 Elsevier Ltd
The authors would like to acknowledge the funding support of this research by the National Natural Science Foundation of China (11871443), Shandong Provincial Qingchuang Science and Technology Project (2019KJI002) and Shandong Provincial Natural Science Foundation (ZR2017MA016). The author (Don) also likes to thank the Ocean University of China for providing the startup funding (201712011) that is used in supporting this work.
PY - 2020/4/30
Y1 - 2020/4/30
N2 - In this work, the characteristic-wise alternative formulation of the seventh and ninth orders conservative weighted essentially non-oscillatory (AWENO) finite difference schemes is derived. The polynomial reconstruction procedure is applied to the conservative variables rather than the flux function of the classical WENO scheme. The numerical flux contains a low order term and high order derivative terms. The low order term can use arbitrary monotone fluxes that can enhance the resolution and reduce numerical dissipation of the fine scale structures while capturing shocks essentially non-oscillatory. The high order derivative terms are approximated by the central finite difference schemes. The improved performance in terms of accuracy, essentially non-oscillatory shock capturing and resolution for the complex shocked flow with fine scale structures in the classical one- and two-dimensional problems is demonstrated. However, the inclusion of the high order derivative terms is prone to generate Gibbs oscillations around a strong discontinuity and might result in a negative density and/or pressure. Therefore, a positivity-preserving limiter [Hu et al. J. Comput. Phys. 242 (2013)] is adopted to ensure the positive density and pressure in the shocked flows with extreme conditions, such as Mach 2000 jet flow problem.
AB - In this work, the characteristic-wise alternative formulation of the seventh and ninth orders conservative weighted essentially non-oscillatory (AWENO) finite difference schemes is derived. The polynomial reconstruction procedure is applied to the conservative variables rather than the flux function of the classical WENO scheme. The numerical flux contains a low order term and high order derivative terms. The low order term can use arbitrary monotone fluxes that can enhance the resolution and reduce numerical dissipation of the fine scale structures while capturing shocks essentially non-oscillatory. The high order derivative terms are approximated by the central finite difference schemes. The improved performance in terms of accuracy, essentially non-oscillatory shock capturing and resolution for the complex shocked flow with fine scale structures in the classical one- and two-dimensional problems is demonstrated. However, the inclusion of the high order derivative terms is prone to generate Gibbs oscillations around a strong discontinuity and might result in a negative density and/or pressure. Therefore, a positivity-preserving limiter [Hu et al. J. Comput. Phys. 242 (2013)] is adopted to ensure the positive density and pressure in the shocked flows with extreme conditions, such as Mach 2000 jet flow problem.
KW - Alternative WENO
KW - Hyperbolic conservation laws
KW - Positivity-preserving
UR - http://www.scopus.com/inward/record.url?scp=85082864153&partnerID=8YFLogxK
UR - https://www.sciencedirect.com/science/article/abs/pii/S004579302030092X?via%3Dihub
U2 - 10.1016/j.compfluid.2020.104519
DO - 10.1016/j.compfluid.2020.104519
M3 - Journal article
AN - SCOPUS:85082864153
SN - 0045-7930
VL - 202
JO - Computers and Fluids
JF - Computers and Fluids
M1 - 104519
ER -