错误 发表于 2025-3-30 09:20:21
http://reply.papertrans.cn/20/1901/190049/190049_51.png改变 发表于 2025-3-30 14:20:43
http://reply.papertrans.cn/20/1901/190049/190049_52.pngcoagulation 发表于 2025-3-30 20:27:00
http://reply.papertrans.cn/20/1901/190049/190049_53.pngChronic 发表于 2025-3-30 21:35:02
Numerical Studies of Higher Order Variational Time Stepping Schemes for Evolutionary Navier-Stokes he evolutionary Navier-Stokes equations. In particular, conforming inf-sup stable pairs of finite element spaces for approximating velocity and pressure are used as spatial discretization while continuous Galerkin–Petrov methods (cGP) and discontinuous Galerkin (dG) methods are applied as higher ordathlete’s-foot 发表于 2025-3-31 02:03:42
Order Reduction and Uniform Convergence of an Alternating Direction Method for Solving 2D Time Depetep discretization process, firstly in space, by using the classical upwind finite difference scheme on a special mesh of Shishkin type, and later on in time by using the fractional implicit Euler method. The method is uniformly convergent with respect to the diffusion parameter having first order iHACK 发表于 2025-3-31 05:03:23
http://reply.papertrans.cn/20/1901/190049/190049_56.pngAprope 发表于 2025-3-31 10:24:22
http://reply.papertrans.cn/20/1901/190049/190049_57.png悲观 发表于 2025-3-31 14:58:19
http://reply.papertrans.cn/20/1901/190049/190049_58.png抱狗不敢前 发表于 2025-3-31 20:12:19
Numerical Calculation of Aerodynamic Noise Generated from an Aircraft in Low Mach Number Flight,fied flap on the wing represented in 2D. Simulation of turbulent flow is modeled using the stabilized orthogonal subgrid scale (OSGS) method with dynamical subscales. It is shown how the stabilization method can perform simulation of turbulent flow affecting the prediction of acoustic sources calculANTI 发表于 2025-4-1 01:32:06
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