標(biāo)題: Titlebook: Computational Fluid Dynamics; Finite Difference Me Guoxiang Hou,Caikan Chen,Kai Wang Book 2024 The Editor(s) (if applicable) and The Author [打印本頁] 作者: Eschew 時(shí)間: 2025-3-21 16:56
書目名稱Computational Fluid Dynamics影響因子(影響力)
作者: Rodent 時(shí)間: 2025-3-21 23:02
Therapie: Methoden und Konzeption,thods for constructing difference schemes are introduced, including Taylor series expansion, method of polynomial interpolation, being-determined coefficient method, integral methods, method?of?characteristics, and control volume method. We provide an example of a one-dimensional advection equation 作者: reperfusion 時(shí)間: 2025-3-22 04:04 作者: 僵硬 時(shí)間: 2025-3-22 08:27 作者: Biomarker 時(shí)間: 2025-3-22 10:13 作者: Chameleon 時(shí)間: 2025-3-22 14:43
Therapie: Methoden und Konzeption,he variable coefficients in linear partial differential equations, if the coefficients of the equation are smooth functions, similar methods to the constant coefficient case can be used to construct difference schemes. The stability and convergence can be analyzed using the frozen coefficient method作者: Chameleon 時(shí)間: 2025-3-22 19:37 作者: SLAY 時(shí)間: 2025-3-23 00:09 作者: 觀察 時(shí)間: 2025-3-23 04:22 作者: calumniate 時(shí)間: 2025-3-23 09:28 作者: invert 時(shí)間: 2025-3-23 10:00 作者: Accede 時(shí)間: 2025-3-23 17:01 作者: forecast 時(shí)間: 2025-3-23 21:27 作者: 租約 時(shí)間: 2025-3-24 02:07 作者: 巨碩 時(shí)間: 2025-3-24 05:36
https://doi.org/10.1007/978-3-540-49759-2hemes, for the discrete unified gas kinetic scheme (DUGKS). The numerical errors of these schemes of no-slip boundary conditions are theoretically analyzed from the view of moment. And numerical performance is assessed and validated by several benchmark problems, such as the Couette flow, the Poiseu作者: Thyroid-Gland 時(shí)間: 2025-3-24 09:59 作者: 薄膜 時(shí)間: 2025-3-24 13:10 作者: chassis 時(shí)間: 2025-3-24 16:39 作者: 獨(dú)白 時(shí)間: 2025-3-24 21:31
Engineering Applications of Computational Methodshttp://image.papertrans.cn/c/image/232291.jpg作者: acheon 時(shí)間: 2025-3-25 02:07
Therapie: Methoden und Konzeption,to illustrate the process. By understanding these methods and concepts, researchers can apply them to other partial differential equations and develop accurate approximate solutions. At the end of this chapter, we give a brief introduction to the difference operator which is a convenient symbol for representing these difference schemes.作者: 不如樂死去 時(shí)間: 2025-3-25 07:06
,Therapie spezieller St?rungsbilder,ete perturbation method, energy method, and Hirt heuristic method, to analyse the numerical stability. Besides, a simple method using difference operator transform to calculate the transition factor is proposed, and an adequate discussion about various forms of stability conditions and the Lax equivalence theorem is given.作者: Ancestor 時(shí)間: 2025-3-25 11:17 作者: Medley 時(shí)間: 2025-3-25 13:56 作者: Foam-Cells 時(shí)間: 2025-3-25 16:09
Therapie: Methoden und Konzeption,dy, the application of slip boundary may also lead to additional drag force as the vortex separation is reduced, which is extremely different from simple channel flows. When the drag reduction materials are applied into practice, the flow state must be considered to achieve the desired effect.作者: harangue 時(shí)間: 2025-3-25 23:39
https://doi.org/10.1007/978-3-540-49759-2ts. Four representative dimensionless heated lengths between 0 and 1, and typical temperature gradient orientations, namely vertical upward are selected to investigate the joint effects of the Richardson number, temperature gradient orientation, and length of the heat source on heat transfer.作者: 亞當(dāng)心理陰影 時(shí)間: 2025-3-26 03:38
https://doi.org/10.1007/978-3-540-49759-2ille flow, the lid-driven cavity flow, and the vortex dipole-wall collision. The results show that the present moment-based scheme is more accurate than the present BB, NEBB, and reference schemes in simulation of Poiseuille flow and dipole-wall collision, compared to the analytical solution and reference data.作者: HALL 時(shí)間: 2025-3-26 06:56 作者: 接觸 時(shí)間: 2025-3-26 10:00
https://doi.org/10.1007/b138224uation and phase velocity change caused by numerical errors are explained. And at the end of this chapter, analysis of numerical oscillations in the short-wave component of solution is implemented to display the influencing factors of numerical oscillation effect.作者: Aphorism 時(shí)間: 2025-3-26 13:13
https://doi.org/10.1007/978-3-540-49759-2undamentals of the LBM are introduced, including the most popular Bhatnagar-Gross-Krook (BGK) model, D2Q9 model for the two dimensions, boundary conditions like the non-equilibrium extrapolation scheme and so on.作者: 自作多情 時(shí)間: 2025-3-26 20:31 作者: 項(xiàng)目 時(shí)間: 2025-3-26 22:25
Numerical Effectuation and phase velocity change caused by numerical errors are explained. And at the end of this chapter, analysis of numerical oscillations in the short-wave component of solution is implemented to display the influencing factors of numerical oscillation effect.作者: Accord 時(shí)間: 2025-3-27 03:03
Fundamentals of Lattice Boltzmann Methodundamentals of the LBM are introduced, including the most popular Bhatnagar-Gross-Krook (BGK) model, D2Q9 model for the two dimensions, boundary conditions like the non-equilibrium extrapolation scheme and so on.作者: 我吃花盤旋 時(shí)間: 2025-3-27 06:45
Book 2024in fluid dynamics. Furthermore, some new ideas are presented in this book, for example, a method to solve the transition matrix by difference operator transformation. For this method, the book gives the definition of Fourier integral transformation of translation operator, and proves the transition 作者: constitute 時(shí)間: 2025-3-27 12:12 作者: 合適 時(shí)間: 2025-3-27 17:37 作者: 半導(dǎo)體 時(shí)間: 2025-3-27 18:37
Therapie: Methoden und Konzeption,iptic stream Poisson equation. And for the velocity–pressure method, we mainly introduce the Maker and Cell method (MAC), which is similar to ordinary difference method in the calculation of difference equation. Then in the last part, the difference method dealing with boundary layer problems is introduced.作者: deviate 時(shí)間: 2025-3-27 22:33 作者: Infelicity 時(shí)間: 2025-3-28 04:33 作者: Adenocarcinoma 時(shí)間: 2025-3-28 07:30
Common Difference Schemes for Several Model Equationsare given, and they are summarized and compared with tables and figures. The advantages and disadvantages of different difference schemes and their application ranges are analyzed, and some issues that need attention are pointed out, such as compatibility, accuracy, computational complexity, and initial conditions.作者: Anterior 時(shí)間: 2025-3-28 12:54 作者: alcohol-abuse 時(shí)間: 2025-3-28 17:11 作者: ETCH 時(shí)間: 2025-3-28 21:49
A Simplified Lattice Boltzmann Flux Solver of Multiphase Flowsg the numerical accuracy and stability of the original MLBFS. We test the simplified MLBFS on the Laplace law and the Rayleigh–Taylor instability problems and show that it can reduce the computation time by up to 18.32% compared to the original method.作者: minion 時(shí)間: 2025-3-29 00:04 作者: engagement 時(shí)間: 2025-3-29 04:48
The Compatibility, Convergence, and Stability of Difference Schemesete perturbation method, energy method, and Hirt heuristic method, to analyse the numerical stability. Besides, a simple method using difference operator transform to calculate the transition factor is proposed, and an adequate discussion about various forms of stability conditions and the Lax equivalence theorem is given.作者: QUAIL 時(shí)間: 2025-3-29 08:20
Variable Coefficients and Nonlinear Problems. For the nonlinear partial differential equations, stability analysis and error estimation for nonlinear problems are more complex than linear problems. At the end of this chapter, the conservative difference scheme is discussed and analyzed using the controlling volume method based on the physical conservation law.作者: Hemodialysis 時(shí)間: 2025-3-29 12:37 作者: 消毒 時(shí)間: 2025-3-29 16:18 作者: Immunotherapy 時(shí)間: 2025-3-29 22:00
Coupled Simplified Lattice Boltzmann Method Study on Thermal Flowsts. Four representative dimensionless heated lengths between 0 and 1, and typical temperature gradient orientations, namely vertical upward are selected to investigate the joint effects of the Richardson number, temperature gradient orientation, and length of the heat source on heat transfer.作者: evanescent 時(shí)間: 2025-3-30 03:21
