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Online since: February 2014
Authors: Da Fei Guo, Ling Zhang, Hui Xia Sheng
            
                Fig .1 The curve of the wind speed changes with height    Fig .2 The flow field area of the wind turbine  
 
   In this paper ,using the method of CFD to build three-dimensional numerical flow field in wind turbine close to the wind turbine operation environment in practice in a greatest degree .Simulation the wind turbine in three-dimensional flows wind shear conditions .
The calculation results and analysis of numerical simulation The output power of wind turbine.
After a fluent numerical simulation.The output calculation results using tecplot to analysis the calculation results.
Research turbulence model horizontal axis wind turbine CFD calculations.
Pre-bend design and numerical simulation of wind turbo-generator [J].Journal of ChineseSociety of Power Engineering, 30(6):450-455.(2010)
            
    The calculation results and analysis of numerical simulation The output power of wind turbine.
After a fluent numerical simulation.The output calculation results using tecplot to analysis the calculation results.
Research turbulence model horizontal axis wind turbine CFD calculations.
Pre-bend design and numerical simulation of wind turbo-generator [J].Journal of ChineseSociety of Power Engineering, 30(6):450-455.(2010)
Online since: October 2010
Authors: Qi Kun Wang
            
                On that basis, a new blade shape called as combined blade for Guiding VAWT was 
proposed and numerical investigation was complemented on its aerodynamic performance by CFD 
(Computational Fluid Dynamics) technique.
CFD (Computational Fluid Dynamics) technique is introduced to numerically investigate the aerodynamic performance of this Guiding VAWT with combined blade.
NUMERICAL MODEL The Guiding VAWT proposed in this paper is essentially a two dimensional structure, so the two dimensional domain for CFD simulation is chosen.
The grids for this CFD calculation is unstructured mesh inside the VAWT while in the extension domain, structure meshes are adopted to reduce the total grid number.
Followings are the prescribed boundary conditions: Inlet: Uniform velocity of the coming flow; Outlet: Ambient pressure of atmosphere; Walls: No-Slip conditions; The whole CFD calculations are complemented by commercial CFD software Fluent and the mesh generation is by its component -GAMBIT.
            
    CFD (Computational Fluid Dynamics) technique is introduced to numerically investigate the aerodynamic performance of this Guiding VAWT with combined blade.
NUMERICAL MODEL The Guiding VAWT proposed in this paper is essentially a two dimensional structure, so the two dimensional domain for CFD simulation is chosen.
The grids for this CFD calculation is unstructured mesh inside the VAWT while in the extension domain, structure meshes are adopted to reduce the total grid number.
Followings are the prescribed boundary conditions: Inlet: Uniform velocity of the coming flow; Outlet: Ambient pressure of atmosphere; Walls: No-Slip conditions; The whole CFD calculations are complemented by commercial CFD software Fluent and the mesh generation is by its component -GAMBIT.
Online since: July 2015
Authors: Yan Jie Li, Ji Hai Jiang, Yun Feng Bai, Jian Zhang
            
                Meanwhile, the single phase of flow field was only considered during the CFD simulation of the hydraulic valves in the above studies, but in fact, the flow field characteristics and cavitation noise of the hydraulic valves were influenced by multi-physics factors.
The hydraulic medium of simulation was 32 # anti-wear hydraulic oil, the opening of the valve port was 5 mm, and other simulation parameters were showed in table 1.
CFD Analysis of Pressure Loss During Flow by Hydraulic Directional Control Valve Constructed from Logic Valves [J].
Simulation of Spool Valve With Notches Based on Fluent [D].
Numerical Simulation of Fluid Flow inside the Valve [J].
            
    The hydraulic medium of simulation was 32 # anti-wear hydraulic oil, the opening of the valve port was 5 mm, and other simulation parameters were showed in table 1.
CFD Analysis of Pressure Loss During Flow by Hydraulic Directional Control Valve Constructed from Logic Valves [J].
Simulation of Spool Valve With Notches Based on Fluent [D].
Numerical Simulation of Fluid Flow inside the Valve [J].
Online since: August 2013
Authors: Wen Long Sun, Xiang Jun Fang, Zhong Ye Wu
            
                ., 2005. parametric and internal study of the vortex tube using CFD model.
Internal study of vortex tube using a CFD package.
J.Refrigeration 33, 783e792. ] used an symmetric CFD model to compare the influence of four different Reynolds- Averaged Navier-Stokes (RANS) based turbulence models (standard k-ε, RNG k-ε, standard k- and SST k-) in predicting the temperature separation.
Simulation of gas species and temperature separation in the counter-flow RanqueeHilsch vortex tube using the large eddy simulation technique.
Heat Mass Transfer 52, 3320e3333. ] used a symmetric CFD model with the LES technique to predict the temperature separation and the separation of nitrogen helium mixture in a VT.
            
    Internal study of vortex tube using a CFD package.
J.Refrigeration 33, 783e792. ] used an symmetric CFD model to compare the influence of four different Reynolds- Averaged Navier-Stokes (RANS) based turbulence models (standard k-ε, RNG k-ε, standard k- and SST k-) in predicting the temperature separation.
Simulation of gas species and temperature separation in the counter-flow RanqueeHilsch vortex tube using the large eddy simulation technique.
Heat Mass Transfer 52, 3320e3333. ] used a symmetric CFD model with the LES technique to predict the temperature separation and the separation of nitrogen helium mixture in a VT.
Online since: December 2010
Authors: Li Li, Zi Dong Hu, Zhi Yuan Cheng
            
                Based on the finite element model and aerodynamic characteristics of the iced conductor, the Runge-Kutta method was applied to carried out non-linear numerical simulation of iced conductor galloping  and the Matlab program was compiled.
In this dissertation, ,a complete set of methods for numerical simulation of galloping has been established based on traditional non-linear finite element method.
The numerical simulation of aerodynamics properties which is based on the computational fluid dynamics(CFD) is developing fast with developing of computer.
The method of numerical simulation has many advantages compared with wind tunnel trial, so ,it is designated by the name of numerical tunnel iconically.
The functional relationship between aerodynamic coefficient an the wind angle of attack can be obtained by the method of numerical simulation, then the nodal wing load can be obtained easily.
            
    In this dissertation, ,a complete set of methods for numerical simulation of galloping has been established based on traditional non-linear finite element method.
The numerical simulation of aerodynamics properties which is based on the computational fluid dynamics(CFD) is developing fast with developing of computer.
The method of numerical simulation has many advantages compared with wind tunnel trial, so ,it is designated by the name of numerical tunnel iconically.
The functional relationship between aerodynamic coefficient an the wind angle of attack can be obtained by the method of numerical simulation, then the nodal wing load can be obtained easily.
Online since: October 2013
Authors: Cheng Chu Yue Fu, Li Li Liu, Shu Ren Yang
            
                Numerical simulation of multi-cup isoflux gas anchor
Physical model creating.
The purpose is to mesh to accurate simulation.
Outputs of numerical simulation Extract useful data for thesis.
[3] P.chow,M.Cross,K.Pericleous.A natural extension of the conventional finite volume method into polygonal unstructured meshes for CFD application[J].App Math Modelling.1996 (20):170-183
[4] L.Suarez,F.Kenyery,M.Asuaje.3D CFD Simulation of Rotary Gas-Separator Performance Under Two-Phase-Flow Condition[C].SPE 94959,2005.
            
    The purpose is to mesh to accurate simulation.
Outputs of numerical simulation Extract useful data for thesis.
[3] P.chow,M.Cross,K.Pericleous.A natural extension of the conventional finite volume method into polygonal unstructured meshes for CFD application[J].App Math Modelling.1996 (20):170-183
[4] L.Suarez,F.Kenyery,M.Asuaje.3D CFD Simulation of Rotary Gas-Separator Performance Under Two-Phase-Flow Condition[C].SPE 94959,2005.
Online since: March 2011
Authors: Jun Tao, Ying Hu, Miao Zhang, Gang Sun
            
                Numerical simulation of N-S equations is employed to obtain near-field acoustic information, then far-field acoustic information is obtained through acoustic analogy theory combined with FW-H equation.
Due to these limitations, the method will eventually be replaced. 3)The method of combining CFD and acoustic analogy.
In this article, the method of combining CFD and acoustic analogy is employed.
To verify the reliability of the flow-field simulation, the dual-element airfoil NLR 7301 is selected to verify the calculation.
Summery Based on numerical simulation of N-S equations, aerodynamic noise prediction of a multi-element airfoil is completed.
            
    Due to these limitations, the method will eventually be replaced. 3)The method of combining CFD and acoustic analogy.
In this article, the method of combining CFD and acoustic analogy is employed.
To verify the reliability of the flow-field simulation, the dual-element airfoil NLR 7301 is selected to verify the calculation.
Summery Based on numerical simulation of N-S equations, aerodynamic noise prediction of a multi-element airfoil is completed.
Online since: May 2014
Authors: Masud Behnia, Rahman T. Nakkas, Babak Fakhim, Ashkan Javadzadegan
            
                Bernad et al [6] has studied the feasibility of using Computational Fluid Dynamics (CFD) to simulate pulsatile blood flow in-vivo in coronary arteries of patients.
However, the main outcome of this study was that it clearly showed that the analysis of transient/pulsatile blood flow using CFD software is indeed feasible in-vivo in realistic coronary artery models, since CFD allows the relevant flow parameters to be characterised with acceptable accuracy.
ANSYS CFX (v14.0, ANSYS-Fluent Inc., Lebanon, NH, USA), a finite volume based software, was coupled to ANSYS Structural (v14.0, ANSYS-Fluent Inc., Lebanon, NH, USA), a finite element based software, for the numerical simulation of the fluid structure interaction (FSI) between the solid (wall) and the fluid (lumen) domains.
Hoffman, Numerical simulations of blood flow in arteries using fluid structure interactions, PhD dissertation, Graduate School of Witchita State University, 2007.
            
    However, the main outcome of this study was that it clearly showed that the analysis of transient/pulsatile blood flow using CFD software is indeed feasible in-vivo in realistic coronary artery models, since CFD allows the relevant flow parameters to be characterised with acceptable accuracy.
ANSYS CFX (v14.0, ANSYS-Fluent Inc., Lebanon, NH, USA), a finite volume based software, was coupled to ANSYS Structural (v14.0, ANSYS-Fluent Inc., Lebanon, NH, USA), a finite element based software, for the numerical simulation of the fluid structure interaction (FSI) between the solid (wall) and the fluid (lumen) domains.
Hoffman, Numerical simulations of blood flow in arteries using fluid structure interactions, PhD dissertation, Graduate School of Witchita State University, 2007.
Online since: September 2014
Authors: Qi Rui Yang, L.H. Piao
            
                By using FLUENT-CFD software, through modeling, meshing, solving and other methods, Respectively, the airflow level posture sensor of two-wire structure and three-wire structure are simulated in the sensitive of the velocity field of different tilt angles and different heat source temperatures.
In order to optimize the airflow level posture sensor heat wire structure, this paper use finite element simulation analysis method to calculate the distribution of sensitive components within the structure of the two air velocity varies with temperature, angle changes.
In order to calculate convenience using ANSYS CFD, the sensitive element is simplified as two dimensional structure, thermal resistance wire and heat source are simplified as points.
First, modeling: choosing ANSYS FLOTRAN CFD analysis function, choosing FLUID141 unit.
            
    In order to optimize the airflow level posture sensor heat wire structure, this paper use finite element simulation analysis method to calculate the distribution of sensitive components within the structure of the two air velocity varies with temperature, angle changes.
In order to calculate convenience using ANSYS CFD, the sensitive element is simplified as two dimensional structure, thermal resistance wire and heat source are simplified as points.
First, modeling: choosing ANSYS FLOTRAN CFD analysis function, choosing FLUID141 unit.
Online since: June 2014
Authors: Wen Yan Li, Shi Yong Wang, Xiao Ming Wang
            
                Numerical calculation about distribution of velocity, NH3 concentration and flow resistance in the deNOx reactor of a 1000MW power plant boiler with CFD have provided the optimal combination of layout scheme of guide plates.
Former study about numerical simulation with Fluent has obtained the best layout scheme of guide devices.
Numerical simulation has acquired the best combination and arrangement of baffles in actual reactor, shown in Fig 2.1.
Table 3.1 Comparison of model test results and numerical simulation consequences Parameter Design requirements results of CFD consequence of model test Note Velocity distribution ±15% 8.3% 11.1% Above the first layer distribution 10% 4.7% 9.8% Above the first layer Total pressure drop 1200Pa 975Pa 980Pa 390Pa pressure loss caused by two catalyst layer It was indicated that model experiment results were very close to numerical simulation results, which suggested that the data investigated met the design requirements.
And during the design process, numerical simulation served as a guide of the model experiment.
            
    Former study about numerical simulation with Fluent has obtained the best layout scheme of guide devices.
Numerical simulation has acquired the best combination and arrangement of baffles in actual reactor, shown in Fig 2.1.
Table 3.1 Comparison of model test results and numerical simulation consequences Parameter Design requirements results of CFD consequence of model test Note Velocity distribution ±15% 8.3% 11.1% Above the first layer distribution 10% 4.7% 9.8% Above the first layer Total pressure drop 1200Pa 975Pa 980Pa 390Pa pressure loss caused by two catalyst layer It was indicated that model experiment results were very close to numerical simulation results, which suggested that the data investigated met the design requirements.
And during the design process, numerical simulation served as a guide of the model experiment.