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Online since: June 2018
Authors: Azzeddine Khorsi, Farouk Kebir
Germain and Baier. [19] Performed numerical simulations on turbine blade channels to identify the flow structure and quantity the secondary flows that are essential for the investigation of losses in a turbine blade channel.
Alameldin et al. [20], performed a CFD Analysis to study the increase in total losses of a transonic turbine blade subjected to film cooling.
The transport equation is additional term utilize to simulates a non-reacting gas mixture when this gases jet in to a cross-flow at different density; the simulations were processed using the CFX software from ANSYS, Inc.
The numerical simulation of the coolant flow through hole system is carried out using the CFD package Ansys CFX coupled with the optimization technique to maximize the film cooling effectiveness.
[16] Lakehal, D., Near-Wall Modeling of Turbulent Convective Heat Transport in Film Cooling of Turbine Blades with the Aid of Direct Numerical Simulation Data.
Alameldin et al. [20], performed a CFD Analysis to study the increase in total losses of a transonic turbine blade subjected to film cooling.
The transport equation is additional term utilize to simulates a non-reacting gas mixture when this gases jet in to a cross-flow at different density; the simulations were processed using the CFX software from ANSYS, Inc.
The numerical simulation of the coolant flow through hole system is carried out using the CFD package Ansys CFX coupled with the optimization technique to maximize the film cooling effectiveness.
[16] Lakehal, D., Near-Wall Modeling of Turbulent Convective Heat Transport in Film Cooling of Turbine Blades with the Aid of Direct Numerical Simulation Data.
Online since: August 2013
Authors: Zheng Lin Liu, Sheng Dong Zhang, Bo Qin, Liang Zhao, Peng Liu
Research on performance of stern shaft mechanical seal based on FLUENT
Peng LIU1, a,Zheng-lin LIU1,b,Sheng-dong Zhang1,c,Bo Qin1,d,Liang Zhao1,e
1School of Energy and Power Engineering, Wuhan University of Technology, Wuhan 430063, China
a 409682311@qq.com,b zlliu812@163.com ,cshengdong.taiji@163.com,
dqb1987616@126.com ,e458378810@qq.com
Keywords: mechanical seal; temperature field; pressure field; CFD
Abstract.Reasonable assumptions and boundary conditions, the application of CFD method of mechanical seal ring structure analysis and thermal - structural coupling analysis,research on the temperature field and the pressure field distribution of the water film between moving and the stationary ring .
In recent years, the development of computational fluid dynamics CFD brings power to seal research.
Khonsari.Numerical Simulations of the Flow Field Aroud the Rings of Mechanical Seals [J].Journal of Tribology;2006,128(7),559-565
In recent years, the development of computational fluid dynamics CFD brings power to seal research.
Khonsari.Numerical Simulations of the Flow Field Aroud the Rings of Mechanical Seals [J].Journal of Tribology;2006,128(7),559-565
Online since: May 2014
Authors: Mohamadreza Nourani, Abbas S. Milani, Spiro Yannacopoulos
Computational Fluid Dynamics (CFD)-based Models
Under this category, some models directly use viscosity laws in simulation and some others are based on an equivalent dynamic viscosity definition from CSM models, also called solid mechanics based dynamic viscosity [2, 16, 19, 30-51].
Multiphysics (CSM-CFD) Models There are models which use both CFD and CSM approaches to predict strains and residual stresses, along with flow characteristics: First they use a CFD approach based on the equivalent dynamic viscosity definition from CSM to predict temperature distribution and the shear stress near tool-material interface.
Xu, Solid mechanics simulation of friction stir welding process, Trans.
Micari, Meshless simulation of friction stir welding.
Wagoner, Numerical simulation of friction stir butt welding process for AA5083-H18 sheets.
Multiphysics (CSM-CFD) Models There are models which use both CFD and CSM approaches to predict strains and residual stresses, along with flow characteristics: First they use a CFD approach based on the equivalent dynamic viscosity definition from CSM to predict temperature distribution and the shear stress near tool-material interface.
Xu, Solid mechanics simulation of friction stir welding process, Trans.
Micari, Meshless simulation of friction stir welding.
Wagoner, Numerical simulation of friction stir butt welding process for AA5083-H18 sheets.
Online since: August 2013
Authors: Guo Xiu Li, Yu Song Yu, Hong Meng Li, Yuan Jing Hou
In this paper, the three-dimensional CFD method is used in numerical simulation of the highly intensified diesel engine intake process.
In the present study, the three-dimensional CFD method is used in numerical simulation of the highly intensified diesel engine intake process.
Double helical Helical and tangential Double tangential Fig.1 Three different combinations of intake port The present simulations focus on the transient process of air inlet, the motion of the valve and piston in the actual work process of diesel engine is used as the input condition.
The simulation begins at the TDC of intake process (360°CA), end up at the end of the intake process (580°CA).
[2]HU Yun-ping, LI Qiu-xia, 3D Transient Numerical Simulation of Flow Field in Cylinder of Diesel Engine with Double-intake Port.
In the present study, the three-dimensional CFD method is used in numerical simulation of the highly intensified diesel engine intake process.
Double helical Helical and tangential Double tangential Fig.1 Three different combinations of intake port The present simulations focus on the transient process of air inlet, the motion of the valve and piston in the actual work process of diesel engine is used as the input condition.
The simulation begins at the TDC of intake process (360°CA), end up at the end of the intake process (580°CA).
[2]HU Yun-ping, LI Qiu-xia, 3D Transient Numerical Simulation of Flow Field in Cylinder of Diesel Engine with Double-intake Port.
Online since: August 2013
Authors: Aminuddin Saat, Mohsin M. Sies, Ghobad Bagheri, Mazlan A. Wahid, Ehsan Hamidi
Results of this simulation show that as the CO2 dilution rate increases, flame temperature and combustion velocity decreases.
Kumar, Numerical simulation of the combustion of hydrogen–air mixture in micro-scaled chambers part II: CFD analysis for a micro-combustor, Chemical engineering science, vol. 60, pp. 3507-3515, 2005
Kumar, Numerical simulation of the combustion of hydrogen–air mixture in micro-scaled chambers.
Vlachos, A CFD study of propane/air microflame stability Combustion and Flame, vol. 138, pp. 97-107, 2004
Vlachos, Combustion characteristics and flame stability at the microscale: a CFD study of premixed methane/air mixtures, Chemical engineering science, vol. 58, pp. 4871-4882, 2003
Kumar, Numerical simulation of the combustion of hydrogen–air mixture in micro-scaled chambers part II: CFD analysis for a micro-combustor, Chemical engineering science, vol. 60, pp. 3507-3515, 2005
Kumar, Numerical simulation of the combustion of hydrogen–air mixture in micro-scaled chambers.
Vlachos, A CFD study of propane/air microflame stability Combustion and Flame, vol. 138, pp. 97-107, 2004
Vlachos, Combustion characteristics and flame stability at the microscale: a CFD study of premixed methane/air mixtures, Chemical engineering science, vol. 58, pp. 4871-4882, 2003
Online since: May 2012
Authors: X.J. Zhao, X.F. Yang, Y.L. Liu, W.L. Wei
Large Eddy Simulation of the Gas–Liquid Flow in a Cylindrical
Cross-Sectioned Bubble Column
W.L.
Numerical Results The simulation example is shown schematically in Figure 1.
Large eddy simulation of con>ned swirling flow.
Computational fluid dynamics (CFD) analysis of multiphase chemical reactors.
Dynamic simulation of dispersed gas–liquid two-phase flow using a discrete bubble model.
Numerical Results The simulation example is shown schematically in Figure 1.
Large eddy simulation of con>ned swirling flow.
Computational fluid dynamics (CFD) analysis of multiphase chemical reactors.
Dynamic simulation of dispersed gas–liquid two-phase flow using a discrete bubble model.
Online since: October 2015
Authors: Zheng Yin Ye, Cheng Xi Zhao, Zi Hang Chen
The other two are designed by an inverse optimization method, which can modify the discrepancies between the CFD (Computational Fluid Dynamics) results and the linearized theory.
The pressure coefficient distributions of the Busemann biplane obtained by CFD technique is given in literature [5] (and).
In the simulation, the conservation form of Euler equations is solved by a finite-volume scheme.
Fig.5(a) shows the configuration of simulations with and .
Fig.5 Simulation model Some aerodynamic forces of different supersonic ring wings are illustrated in Table1 with and .
The pressure coefficient distributions of the Busemann biplane obtained by CFD technique is given in literature [5] (and).
In the simulation, the conservation form of Euler equations is solved by a finite-volume scheme.
Fig.5(a) shows the configuration of simulations with and .
Fig.5 Simulation model Some aerodynamic forces of different supersonic ring wings are illustrated in Table1 with and .
Online since: March 2010
Authors: Jian Min Wu
The electrolyte flow channel was used as
numerical simulation physical model.
Numerical simulation of workpiece surface speed distribution was carried out with different cathode outlet slot structure by using Computational Fluid Dynamics (CFD).
Mesh quality directly affects numerical simulation results of the flow field.
Therefore, the numerical simulation was performed with different inlet pressures and fixed inter-electrode gap (∆ = 0.5mm).
Wang: Computational fluid dynamics analysis - CFD Software Theory and Application (Tsinghua University Press, Beijing 2004)
Numerical simulation of workpiece surface speed distribution was carried out with different cathode outlet slot structure by using Computational Fluid Dynamics (CFD).
Mesh quality directly affects numerical simulation results of the flow field.
Therefore, the numerical simulation was performed with different inlet pressures and fixed inter-electrode gap (∆ = 0.5mm).
Wang: Computational fluid dynamics analysis - CFD Software Theory and Application (Tsinghua University Press, Beijing 2004)
Online since: June 2012
Authors: Fu Sheng Li, Xin Xi Xu, Ya Jun Liu, Shu Lin Tan, Dong Sun
Numerical Simulation Study on Airflow Structural Characteristics in Real Human Airways Model
SUN Dong1,a, LI Fu-Sheng1,b, XU Xin-Xi1,c, LIU Ya-Jun1, TAN Shu-Lin1
1Institute of Medical Equipment, Academy of Military Medicine Sciences; National Biological Protection Engineering Center, Tianjin 300161 China
axizhilang-dongdong@163.com, bfsisok@163.com, cxuxx1@sohu.com
c.
Corresponding author,Tel:022-84656705; E-mail:xuxx1@sohu.com Keywords: human airways; transient airflow movement; airflow patterns; numerical simulation Abstract.
In this paper, the SST simulation was used to simulate precise flow field in human upper respiratory tract in the conditions of the low intensive respiratory patterns.
Because of this, it can be coupled with CFD code.
The former is coupled with SST turbulence model which is used to open the turbulent kinetic energy in the downstream of turning point in order to trigger the local transition; the latter is used to catch the influence of offsite turbulence intensity and also connect the empirical correlation with the transition starting standards intermittent factor transport equations. 1.3 Numerical simulation In the computing of the flow field, its boundary conditions we set are: we conduct simulation researches on transient airflow movement in model of mouth-throat under the low intensity circular breathing mode.
Corresponding author,Tel:022-84656705; E-mail:xuxx1@sohu.com Keywords: human airways; transient airflow movement; airflow patterns; numerical simulation Abstract.
In this paper, the SST simulation was used to simulate precise flow field in human upper respiratory tract in the conditions of the low intensive respiratory patterns.
Because of this, it can be coupled with CFD code.
The former is coupled with SST turbulence model which is used to open the turbulent kinetic energy in the downstream of turning point in order to trigger the local transition; the latter is used to catch the influence of offsite turbulence intensity and also connect the empirical correlation with the transition starting standards intermittent factor transport equations. 1.3 Numerical simulation In the computing of the flow field, its boundary conditions we set are: we conduct simulation researches on transient airflow movement in model of mouth-throat under the low intensity circular breathing mode.
Online since: June 2014
Authors: Krishna Murari Pandey, Sukanta Roga
CFD Analysis of Scramjet Combustor with Non-Premixed Turbulence Model Using Ramp Injector
K.M.
Schumacher [10] studied the Numerical Simulation of Cantilevered Ramp Injector Flow Fields for Hyper velocity Fuel-Air Mixing Enhancement.
Schumacher, Numerical Simulation of Cantilevered Ramp Injector Flow Fields for Hypervclocity Fuel-Air Mixing Enhancement, Ph.D.
Sivasakthivel, CFD Analysis of Mixing and Combustion of a Hydrogen Fueled Scramjet Combustor with a Strut Injector by Using Fluent Software, IACSIT International Journal of Engineering and Technology, Vol. 3, No. 5, (October 2011)
Singh, CFD Analysis of Supersonic Combustion Using Diamond Shaped Strut Injector With standard K-Є Non-Premixed Turbulence Model, International Journal of Advanced Trends in Computer Science and Engineering, Volume 1 No.-1, PP. 33-42, (March- April 2012).
Schumacher [10] studied the Numerical Simulation of Cantilevered Ramp Injector Flow Fields for Hyper velocity Fuel-Air Mixing Enhancement.
Schumacher, Numerical Simulation of Cantilevered Ramp Injector Flow Fields for Hypervclocity Fuel-Air Mixing Enhancement, Ph.D.
Sivasakthivel, CFD Analysis of Mixing and Combustion of a Hydrogen Fueled Scramjet Combustor with a Strut Injector by Using Fluent Software, IACSIT International Journal of Engineering and Technology, Vol. 3, No. 5, (October 2011)
Singh, CFD Analysis of Supersonic Combustion Using Diamond Shaped Strut Injector With standard K-Є Non-Premixed Turbulence Model, International Journal of Advanced Trends in Computer Science and Engineering, Volume 1 No.-1, PP. 33-42, (March- April 2012).