標(biāo)題: Titlebook: Boundary Elements in Fluid Dynamics; C. A. Brebbia,P. W. Partridge Book 1992 Computational Mechanics Publications 1992 computational fluid [打印本頁] 作者: 使作嘔 時(shí)間: 2025-3-21 19:23
書目名稱Boundary Elements in Fluid Dynamics影響因子(影響力)
書目名稱Boundary Elements in Fluid Dynamics影響因子(影響力)學(xué)科排名
書目名稱Boundary Elements in Fluid Dynamics網(wǎng)絡(luò)公開度
書目名稱Boundary Elements in Fluid Dynamics網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Boundary Elements in Fluid Dynamics被引頻次
書目名稱Boundary Elements in Fluid Dynamics被引頻次學(xué)科排名
書目名稱Boundary Elements in Fluid Dynamics年度引用
書目名稱Boundary Elements in Fluid Dynamics年度引用學(xué)科排名
書目名稱Boundary Elements in Fluid Dynamics讀者反饋
書目名稱Boundary Elements in Fluid Dynamics讀者反饋學(xué)科排名
作者: 口訣 時(shí)間: 2025-3-21 21:25
https://doi.org/10.1007/b138241 possible modification to the original design has been looked at and an optimum design was selected. This method is found to be economical in this initial design and optimisation process, which will vastly reduce the amount of wind tunnel work and road-tests required.作者: Pageant 時(shí)間: 2025-3-22 04:07
https://doi.org/10.1007/978-3-211-75794-9 averaged form of the Navier-Stokes equations is employed through the Reynolds decomposition of the instantaneous value of each variable. Turbulent stress terms are interpreted in the Boussinesq manner and Prandtl’s mixing length hypothesis is used. Only algebraic turbulent model is considered in this paper.作者: SMART 時(shí)間: 2025-3-22 04:51 作者: 傀儡 時(shí)間: 2025-3-22 12:37 作者: Aprope 時(shí)間: 2025-3-22 13:10 作者: Acquired 時(shí)間: 2025-3-22 17:18
The Boundary Element Solution of a Viscous Free Surface ProblemIn this paper we use the boundary element method to solve a very slow viscous flow with a free surface. An iterative scheme is developed and the numerical solutions are obtained for various non-dimensional fluid flow rates, q, and the non-dimensional surface tension, T.作者: 愛社交 時(shí)間: 2025-3-22 23:45 作者: 打算 時(shí)間: 2025-3-23 01:40
Computational Mechanics Publications 1992作者: 巫婆 時(shí)間: 2025-3-23 09:06 作者: 獨(dú)特性 時(shí)間: 2025-3-23 13:28 作者: Fibrinogen 時(shí)間: 2025-3-23 15:31 作者: Capture 時(shí)間: 2025-3-23 18:10 作者: 斜谷 時(shí)間: 2025-3-23 22:33
https://doi.org/10.1007/b138241tization element. In order to improve accuracy, Nixon [1] assumed that within the discretization element the dependent variable was constant in the streamwise direction but varied linearly in the transverse direction. Ogana [2–7] has made a similar assumption but has formulated the problem in more g作者: Concerto 時(shí)間: 2025-3-24 03:05 作者: 金桌活畫面 時(shí)間: 2025-3-24 08:28 作者: boisterous 時(shí)間: 2025-3-24 14:44 作者: angiography 時(shí)間: 2025-3-24 16:23 作者: GUILT 時(shí)間: 2025-3-24 19:44 作者: babble 時(shí)間: 2025-3-25 02:31
https://doi.org/10.1007/978-94-009-0281-7velocity values from the momentum conservation using the Galerkin Finite Element discretization in space. The Poisson’s equation is solved for a derived scalar variable to evaluate the pressure field at each time step. For imposing the far field boundary conditions on pressure approximate boundary e作者: 旅行路線 時(shí)間: 2025-3-25 04:21
Low Temperature Molecular Spectroscopy bodies. Small-amplitude waves and motions and irrotational flow are assumed and the resulting linear problem is solved in the frequency domain with six degrees of freedom of each body. The developed computer programme is made efficient by using the Haskind relation for the calculation of forces and作者: Allure 時(shí)間: 2025-3-25 08:41
Introduction to strongly correlated systems, formulation, which is very suitable for the boundary conditions involved. The displacement of the moving surface is calculated explicitly; smoothing and regridding insure stability of the overall scheme. The method allows one to simulate directly the behavior of very thin dynamic films left behind 作者: 敬禮 時(shí)間: 2025-3-25 12:11
http://image.papertrans.cn/b/image/190012.jpg作者: dissent 時(shí)間: 2025-3-25 15:50 作者: 浮夸 時(shí)間: 2025-3-25 19:58
Investigation of the Aerodynamic Performance of a Formula 1 Multi-Aerofoil Spoiler using a Second Or possible modification to the original design has been looked at and an optimum design was selected. This method is found to be economical in this initial design and optimisation process, which will vastly reduce the amount of wind tunnel work and road-tests required.作者: 憲法沒有 時(shí)間: 2025-3-26 00:58 作者: 充滿人 時(shí)間: 2025-3-26 08:14
The Complete Double Layer Boundary Integral Equation Method for Particles Moving Close to Boundariesses a unique continuous solution when the boundary of the particle is a Lyapunov surface and the velocity data on the boundary surface is continuous and this system is used as the basis of a numerical model that uses standard boundary element techniques.作者: 小平面 時(shí)間: 2025-3-26 11:46
3-D Time Dependent Navier-Stokes Solutions with Finite and Boundary Elementslement concept external to the finite element region is utilized. Presented are the numerical results obtained for viscous flow past a swept bump on a circular cylinder. The technique proves itself to be capable of depicting the flow field with small number of grid points used in discretization in space and with considerably large steps in time.作者: 緩解 時(shí)間: 2025-3-26 12:45
Modelling of Seas and Coastal Regions and Boundary Elements and Fluid Dynamics, held in Southampton, U.K., in April 1992. The Boundary Element Method (BEM) is now fully established as an ac- curate and successful technique for solving engineering problems in a wide range of fields. The success of t作者: 哀求 時(shí)間: 2025-3-26 17:53 作者: omnibus 時(shí)間: 2025-3-26 22:53
Introduction to strongly correlated systems,and regridding insure stability of the overall scheme. The method allows one to simulate directly the behavior of very thin dynamic films left behind a receding meniscus. The numerical results are compared with both experimental observations and calculations based on a simplified theoretical analysis.作者: 不在灌木叢中 時(shí)間: 2025-3-27 04:09
A Numerical Simulation of Cross Flow Fanrtex distributions on the boundaries and blades, and free vortices shed from the impeller blades following Kelvin’s circulation theorem. Numerical simulation results are in good agreement with experimental results.作者: 消息靈通 時(shí)間: 2025-3-27 07:08 作者: Budget 時(shí)間: 2025-3-27 09:56 作者: Infant 時(shí)間: 2025-3-27 13:43 作者: 配置 時(shí)間: 2025-3-27 18:58 作者: ureter 時(shí)間: 2025-3-27 23:51 作者: 預(yù)兆好 時(shí)間: 2025-3-28 02:40
Including Sharp Edge Vortex Shedding in Boundary Integral Solutions for Two Dimensional Potential Fl the inner region solution to the problem of flow past the normal plate. This inner region solution has to be matched with the outer potential flow solution. The combination of boundary element and discrete vortex methods provides this matching and at the same time do not require calculations inside the domain.作者: 從屬 時(shí)間: 2025-3-28 06:25
Hydrodynamic Properties of Multiple Floating and Submerged Bodies Analysed by a Panel Methodand motions calculated by the method of expansion in matched eigenfunctions. The agreement is good..As practical applications, the effect of offset between buoy and plate and the effect of the shape of the buoy and plate are investigated..The programme is coded in FORTRAN 77 and is presently run on a PC 386.作者: 動物 時(shí)間: 2025-3-28 10:40
https://doi.org/10.1007/b138241g rise to “hybrid” elements for both the integral and integro-differential equations. These methods yield improved accuracy but they cannot be conveniently applied to a large computational domain without a sharp increase in nodes and discretization elements.作者: 無能力 時(shí)間: 2025-3-28 15:56 作者: 諄諄教誨 時(shí)間: 2025-3-28 21:59 作者: 保存 時(shí)間: 2025-3-28 23:21
https://doi.org/10.1007/978-3-211-75794-9ses a unique continuous solution when the boundary of the particle is a Lyapunov surface and the velocity data on the boundary surface is continuous and this system is used as the basis of a numerical model that uses standard boundary element techniques.作者: BOOM 時(shí)間: 2025-3-29 05:18
https://doi.org/10.1007/978-94-009-0281-7lement concept external to the finite element region is utilized. Presented are the numerical results obtained for viscous flow past a swept bump on a circular cylinder. The technique proves itself to be capable of depicting the flow field with small number of grid points used in discretization in space and with considerably large steps in time.作者: Chronological 時(shí)間: 2025-3-29 08:44
https://doi.org/10.1007/b138241linear compressible flows. To be consistent with the mixed-nature of transonic flows, the Murman-Cole type-difference scheme is used to compute the derivatives of the density. The present scheme is applied to flows around a rectangular wing with circular-arc section at incompressible, high- subsonic作者: WAX 時(shí)間: 2025-3-29 14:59
https://doi.org/10.1007/b138241ional flow around an airfoil is considered, in which the boundary layer separates from the airfoil and an adjacent dead air region is formed. As second example, the flow around a prolate spheroid at incidence is treated, in which case separation leads to a thin free vortex layer. A third example is 作者: 缺乏 時(shí)間: 2025-3-29 17:39 作者: 圣人 時(shí)間: 2025-3-29 22:02
rious test for any numerical method, and is an area in which BEM analysis may be used taking full advantage of its special characteris- tics. The conference includes sections on turbomachinery, aerodynamics, viscous flow and turbulence models, and special flow situations. The organisers would like to thank th978-94-011-2876-6作者: facetious 時(shí)間: 2025-3-30 01:07
A 3D IEM for Compressible Wing Flows With and Without Shockslinear compressible flows. To be consistent with the mixed-nature of transonic flows, the Murman-Cole type-difference scheme is used to compute the derivatives of the density. The present scheme is applied to flows around a rectangular wing with circular-arc section at incompressible, high- subsonic作者: 巨頭 時(shí)間: 2025-3-30 06:05
Description of Viscous-Inviscid Interaction Using Boundary Elementsional flow around an airfoil is considered, in which the boundary layer separates from the airfoil and an adjacent dead air region is formed. As second example, the flow around a prolate spheroid at incidence is treated, in which case separation leads to a thin free vortex layer. A third example is 作者: allergy 時(shí)間: 2025-3-30 09:49 作者: paroxysm 時(shí)間: 2025-3-30 13:49
Fully 3D Euler Solutions Versus Test Results for the Whole Load Range of Radial Pumpsomparisons with the theoretical head derived from test results have yielded a nearly 50% reduction against the scatter band width of empirical correlation methods..Part load flow patterns have been calculated for the range between shut off and the best efficiency point. Realistic velocity profiles h作者: Exposure 時(shí)間: 2025-3-30 16:58
Experience with Transonic Flow IE Computationsin the moving frame of reference, in the form of the Poisson’s equation. The integral equation solution in terms of the velocity field is obtained by the Green’s theorem. The mixed nature of the transonic flow is treated by a type- difference scheme. The numerical solutions are obtained by a time-ma作者: Coronary 時(shí)間: 2025-3-30 21:49 作者: nullify 時(shí)間: 2025-3-31 01:47 作者: 全神貫注于 時(shí)間: 2025-3-31 06:32
