標(biāo)題: Titlebook: Computational Fluid Dynamics for the 21st Century; Proceedings of a Sym Mohamed Hafez,Koji Morinishi,Jacques Periaux Conference proceedings [打印本頁] 作者: Monsoon 時間: 2025-3-21 19:59
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書目名稱Computational Fluid Dynamics for the 21st Century讀者反饋
書目名稱Computational Fluid Dynamics for the 21st Century讀者反饋學(xué)科排名
作者: 意見一致 時間: 2025-3-21 22:31
Asymptotic behavior of stochastic automata,ctice in an industrial setting, the design approach presented in this paper can yield large computational savings as well as reduced turn around times that can be used to either decrease the time to market or to increase the number of design iterations within a given time frame.作者: assent 時間: 2025-3-22 00:46 作者: Cloudburst 時間: 2025-3-22 08:10 作者: 驚惶 時間: 2025-3-22 09:03 作者: FECT 時間: 2025-3-22 14:34 作者: FECT 時間: 2025-3-22 20:53
Isotropic and Anisotropic Adaptive Meshes : Models and Convergence Propertiessented in the simplified case of mesh adaptive interpolation or compression. We dedicate this work to Professor Satofuka, expressing our admiration for the work of the scientist and our friendliness for our colleague.作者: Cubicle 時間: 2025-3-22 22:04
https://doi.org/10.1007/978-981-99-8277-6e solver can work fairly well on the points of any kind of grids and even on points arbitrarily distributed over the computational domains. The flexibility and reliability of the present method are demonstrated for representative test cases of subsonic, transonic, and supersonic flows.作者: BRINK 時間: 2025-3-23 05:20 作者: 青少年 時間: 2025-3-23 09:19
Harold J. Kushner,G. George Yinrved that the hairpin vortex ring is released and the flow transits from laminar to turbulence in . = 1000. It is shown in the flow around two spheres that the released vortex rings interfere each other. Consequently, the present method is very promising for the DNSs of the incompressible complicated flow.作者: esthetician 時間: 2025-3-23 11:57 作者: effrontery 時間: 2025-3-23 14:32 作者: handle 時間: 2025-3-23 18:34 作者: 無能力 時間: 2025-3-23 22:52 作者: CLASP 時間: 2025-3-24 05:08
Cartesian Grid Approach with Virtual Boundary Method and Its Applicationsrved that the hairpin vortex ring is released and the flow transits from laminar to turbulence in . = 1000. It is shown in the flow around two spheres that the released vortex rings interfere each other. Consequently, the present method is very promising for the DNSs of the incompressible complicated flow.作者: output 時間: 2025-3-24 07:39
A second-order-accurate fluctuation splitting scheme for unsteady hyperbolic problemsn equation is considered for simplicity. Again, a predictor-corrector scheme is proposed, which combines a first-orderaccurate FS predictor step with a flux-corrected-transport LW corrector one..Standard test problems are used to verify the accuracy of the proposed schemes.作者: Arthritis 時間: 2025-3-24 12:08
Genetic Algorithms and Game Theory for High Lift Multi-Airfoil Design Problems in Aerodynamicsto high lift multi-airfoil design. Numerical results obtained with this new approach are compared favorably with single global GAs’ ones and illustrate the promising robustness and efficient parallel properties of coupled GAs with different game scenarios for future advanced multidisciplinary aerospace technologies.作者: abject 時間: 2025-3-24 17:16 作者: ECG769 時間: 2025-3-24 21:34 作者: Stricture 時間: 2025-3-25 02:24 作者: 透明 時間: 2025-3-25 06:33 作者: 新鮮 時間: 2025-3-25 08:34 作者: 合群 時間: 2025-3-25 14:23
S. Albeverio,Ph. Blanchard,R. H?egh-Krohnlic problems including compressible flows with shocks. The DNC and RBC schemes produce high-order results, but the RBC scheme proves to be much better for shock capturing capabilities and computational efficiency.作者: 令人發(fā)膩 時間: 2025-3-25 17:14
Residual-Based Compactness versus Directionality for High-Order Compressible Flow Calculationslic problems including compressible flows with shocks. The DNC and RBC schemes produce high-order results, but the RBC scheme proves to be much better for shock capturing capabilities and computational efficiency.作者: corn732 時間: 2025-3-25 21:58
Cartesian Grid Approach with Virtual Boundary Method and Its Applicationsthe body surface is expressed by a set of plural points, and the velocity components on virtual boundary are feedbacked to the momentum equations as the additional forcing terms. In order to validate the present method, the DNSs of flow around a circular cylinder are considered. The flow characteris作者: deadlock 時間: 2025-3-26 01:45 作者: 英寸 時間: 2025-3-26 08:06 作者: 假設(shè) 時間: 2025-3-26 12:31 作者: DEFT 時間: 2025-3-26 14:05
Progress in the Development of a Class of Efficient Low Dissipative High Order Shock-Capturing Metho Yee (2000), the issue of nonlinear stability of the compressible Euler and Navier-Stokes Equations, including physical boundaries, and the corresponding development of the discrete analogue of nonlinear stable high order schemes, including boundary schemes, were developed, extended and evaluated fo作者: 連鎖,連串 時間: 2025-3-26 19:03
A second-order-accurate fluctuation splitting scheme for unsteady hyperbolic problemsStokes) equations, to the case of unsteady flows. Two slightly different approaches are proposed for the one- and two-dimensional flow-cases, respectively..For the one-dimensional Euler equations, a predictor-corrector scheme is proposed, which combines a first-order-accurate FS scheme at the predic作者: LAIR 時間: 2025-3-26 22:17
Lattice-Boltzmann Methods — A New Tool in CFDns of different types and for local grid refinement. Wide spread applications show the performance of the lattice-Boltzmann concept, ranging from gas-particle flows to turbulent flows and combustion processes.作者: AWE 時間: 2025-3-27 04:51 作者: Visual-Field 時間: 2025-3-27 06:36
Multi-Objective Aerodynamic and Aeroelastic Optimizationf the exposed X31 delta wing. Results are achieved by means of a multi-objective genetic algorithm (GA) utilizing a GUI-supported software being developed in the European-Union funded “FRONTIER” project.作者: FID 時間: 2025-3-27 12:38
Genetic Algorithms and Game Theory for High Lift Multi-Airfoil Design Problems in Aerodynamicsfoil systems in Aerospace Engineering. GAs are IT based evolutionary methods introduced by J.H. Holland for mimicking natural adaptation systems in the computer. Due to large dimension global optimization problems and the increasing importance of low cost distributed parallel environments it is a na作者: placebo 時間: 2025-3-27 14:07
Parallel Computation of Flow Problems Using Explicit Schemesed with computation and communication costs. Data parallelization is assumed where the flow domain is divided into sub-regions (blocks) which are connected to each other by smaller sub-regions (interfaces). In order to reduce the computation cost, two approaches are proposed: an explicit block solve作者: 綠州 時間: 2025-3-27 18:55
Parallel Computation of Compressible Flows for Implicit Schemes Without Sub-iteration and Modificatiury for handling large scale problems. Implicit schemes are efficient for obtaining steady state solutions and for treating slowly unsteady flows. However, implicit schemes are not inherently parallel and their parallelization usually requires addtional iteration or modification of the implicit solv作者: 割讓 時間: 2025-3-28 01:17 作者: 盡忠 時間: 2025-3-28 04:59 作者: 抑制 時間: 2025-3-28 08:12
Mohamed Hafez,Koji Morinishi,Jacques PeriauxNew trends in Computational Fluid Dynamics, especially useful to the younger generation of scientists and engineers in the field..Includes supplementary material: 作者: 圣人 時間: 2025-3-28 11:41
Notes on Numerical Fluid Mechanics and Multidisciplinary Designhttp://image.papertrans.cn/c/image/232308.jpg作者: 美色花錢 時間: 2025-3-28 16:17
Lattice-Boltzmann Methods — A New Tool in CFDns of different types and for local grid refinement. Wide spread applications show the performance of the lattice-Boltzmann concept, ranging from gas-particle flows to turbulent flows and combustion processes.作者: GRE 時間: 2025-3-28 22:10 作者: 客觀 時間: 2025-3-28 23:48
Computational Fluid Dynamics for the 21st Century978-3-540-44959-1Series ISSN 1612-2909 Series E-ISSN 1860-0824 作者: 粗俗人 時間: 2025-3-29 04:39
Diffusions and central limit theorems,ns of different types and for local grid refinement. Wide spread applications show the performance of the lattice-Boltzmann concept, ranging from gas-particle flows to turbulent flows and combustion processes.作者: lethargy 時間: 2025-3-29 08:07 作者: 食道 時間: 2025-3-29 12:25
Weak Convergence: Introduction,Over the last three decades, Prof. Satofuka made many important contributions to Computational Fluid Dynamics (CFD). In this article, after a brief introduction, some of his work will be discussed, and a complete list of his publications (through December 1999) is included for the record.作者: pacific 時間: 2025-3-29 17:34 作者: 拘留 時間: 2025-3-29 23:37 作者: FLIC 時間: 2025-3-30 03:49 作者: 制造 時間: 2025-3-30 07:59
https://doi.org/10.1007/978-981-99-8277-6f grids, are first distributed over the computational domain considered. The spatial derivatives of flow quantities are evaluated at each point with linear combinations of certain coefficients and the quantities in its cloud of points. An upwind method may be obtained using Roe’s approximate Riemann作者: 詞根詞綴法 時間: 2025-3-30 11:16 作者: 斑駁 時間: 2025-3-30 12:47
https://doi.org/10.1007/BFb0101532 Yee (2000), the issue of nonlinear stability of the compressible Euler and Navier-Stokes Equations, including physical boundaries, and the corresponding development of the discrete analogue of nonlinear stable high order schemes, including boundary schemes, were developed, extended and evaluated fo作者: Calculus 時間: 2025-3-30 18:10
Ergodic properties of the Lozi map,Stokes) equations, to the case of unsteady flows. Two slightly different approaches are proposed for the one- and two-dimensional flow-cases, respectively..For the one-dimensional Euler equations, a predictor-corrector scheme is proposed, which combines a first-order-accurate FS scheme at the predic作者: Tailor 時間: 2025-3-31 00:37
