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Online since: February 2014
Authors: Ting Yu, Feng Qi Yu, Ben Xian Peng
ANSYS and SPICE simulation results show that the proposed sensor can worked properly under 500K Pa, and the square sensing membrane of 100x100 mm 2 shows a good linearity over a pressure change ranging from 5 Pa to 500K Pa.
The total capacitors include Cfd, Cfs, Cfd and Cfb.
Main electrical parameters for SPICE simulation are shown below: channel length is 20mm, channel width is 50 mm, equivalent gate oxide thickness is 3.7 nm, channel doping density is 1.1´1015/cm2, and threshold voltage is -34.19 mV.
Fig.5 SPICE simulation results of the drain current with different pressure Summary In this paper, a floating-gate MOSFET pressure sensor with floating gate has been proposed, and the operation principle of the device in standard CMOS process has been discussed.
ANSYS and SPICE simulation results show that the proposed sensor can worked properly under 500K Pa, and the square sensing membrane of 100x100 mm 2 shows a good linearity over a pressure change ranging from 5 Pa to 500K Pa.
The total capacitors include Cfd, Cfs, Cfd and Cfb.
Main electrical parameters for SPICE simulation are shown below: channel length is 20mm, channel width is 50 mm, equivalent gate oxide thickness is 3.7 nm, channel doping density is 1.1´1015/cm2, and threshold voltage is -34.19 mV.
Fig.5 SPICE simulation results of the drain current with different pressure Summary In this paper, a floating-gate MOSFET pressure sensor with floating gate has been proposed, and the operation principle of the device in standard CMOS process has been discussed.
ANSYS and SPICE simulation results show that the proposed sensor can worked properly under 500K Pa, and the square sensing membrane of 100x100 mm 2 shows a good linearity over a pressure change ranging from 5 Pa to 500K Pa.
Online since: August 2012
Authors: Bai Ping Xu, Hui Wen Yu
This work aims at simulation of the mixing performance in the novel co-rotating non-twin screw group developed by the authors.
The simulation concerns the incompressible fluid obeying Carreau flow model.
To the best of our knowledge, numerical simulations about such mixing sections are still rare.
Finite element method (FEM) simulations were carried out by the commercially available CFD software Polyflow by Fluent Inc., using a mixed Galerkin formulation of the isothermal governing equations: (1) (2) Whereis the velocity vector, is the stress tensor, p is the pressure.
Time periodicity and geometry of such a group with the speed ratio equal to 2 are described in the simple way to show what goes on during operating. 2D numerical simulation of flow and mixing in such mixing section is carried out adapting the commercial CFD FEM package Polyflow.
The simulation concerns the incompressible fluid obeying Carreau flow model.
To the best of our knowledge, numerical simulations about such mixing sections are still rare.
Finite element method (FEM) simulations were carried out by the commercially available CFD software Polyflow by Fluent Inc., using a mixed Galerkin formulation of the isothermal governing equations: (1) (2) Whereis the velocity vector, is the stress tensor, p is the pressure.
Time periodicity and geometry of such a group with the speed ratio equal to 2 are described in the simple way to show what goes on during operating. 2D numerical simulation of flow and mixing in such mixing section is carried out adapting the commercial CFD FEM package Polyflow.
Online since: February 2012
Authors: Dun Zhang, Yuan Zheng
Coupled with the rapid development of CFD (Computational Fluid Dynamics) technology, numerical simulation for the cavitations flows, both can make up the shortcomings of theoretical analysis methods in complex cavitations problems applications and also save the cost of model test, moreover it can be accuracy, high speed, and can simulate the pattern of the flow field and get accurate flow characteristics without the impact the constraints inherent in testing.
The Physical model of simulation The simulation is for a model full-flow of the giant unit, which over-current components are: scroll, vanes, guide vanes, runner, draft tube.
Before the unsteady simulation, the standard k-ε model was used for the steady simulation, and the flow data upon steady simulation with will be as the initial conditions for the unsteady simulation.
The unsteady simulation will use the RNG k-ε model.
A CFD parametric study of geometrical variations on the pressure pulsations and performance characteristics of a centrifugal pump.
The Physical model of simulation The simulation is for a model full-flow of the giant unit, which over-current components are: scroll, vanes, guide vanes, runner, draft tube.
Before the unsteady simulation, the standard k-ε model was used for the steady simulation, and the flow data upon steady simulation with will be as the initial conditions for the unsteady simulation.
The unsteady simulation will use the RNG k-ε model.
A CFD parametric study of geometrical variations on the pressure pulsations and performance characteristics of a centrifugal pump.
Online since: August 2013
Authors: Yong Ling Fu, Zhu Feng Li, Xiao Ning Zhang, Jing Xue
Finally we do simulations in ANSYS.
Second is performance simulation.
The flow field of a new axial piston EHP is studied based on CFD in Ref.[11], including the models of main flow fields of the pump, numerical simulations, the velocity and pressure distribution.
Simulation and Results Simulation Conditions.
Simulations.
Second is performance simulation.
The flow field of a new axial piston EHP is studied based on CFD in Ref.[11], including the models of main flow fields of the pump, numerical simulations, the velocity and pressure distribution.
Simulation and Results Simulation Conditions.
Simulations.
Online since: October 2011
Authors: Xiu Lan Huai, Da Wei Tang, Zhao Yin Wen, Zhao Yi Dong, Zhi Gang Li
Numerical simulation is performed for the two-dimensional axisymmetric domain of a single cell.
The simulation results of the transient temperature fields provide useful guidance for the optimized thermal design so as to enhance the energy efficiency of the battery system.
The equations of species transport and heat transfer are solved by a commercial CFD code FLUENT based on a Finite Volume (FV) method.
The coupling of the electrochemical equations to the CFD code is implemented by loading and executing a set of User Defined Functions (UDFs).
(4) The simulation results of the temperature fields are useful for the optimized design of the thermal management system and for enhancing the battery energy efficiency.
The simulation results of the transient temperature fields provide useful guidance for the optimized thermal design so as to enhance the energy efficiency of the battery system.
The equations of species transport and heat transfer are solved by a commercial CFD code FLUENT based on a Finite Volume (FV) method.
The coupling of the electrochemical equations to the CFD code is implemented by loading and executing a set of User Defined Functions (UDFs).
(4) The simulation results of the temperature fields are useful for the optimized design of the thermal management system and for enhancing the battery energy efficiency.
Online since: November 2012
Authors: Yao Hua Zhao, Feng Wang
The study methods mainly include numerical simulation and experimental study.
Due to the advantages such as fastness, accuracy, low cost and strong operability and so on, the numerical simulation is widely applied.
Simulation object and model establishment Type of transfer stations.
Simulation object.
The physical model is seen in figure 1, and numerical simulation study is conducted on the smoke diffusion rule by adopting CFD simulation software ANSYS CFX11.0 when the fire occurs.
Due to the advantages such as fastness, accuracy, low cost and strong operability and so on, the numerical simulation is widely applied.
Simulation object and model establishment Type of transfer stations.
Simulation object.
The physical model is seen in figure 1, and numerical simulation study is conducted on the smoke diffusion rule by adopting CFD simulation software ANSYS CFX11.0 when the fire occurs.
Online since: February 2017
Authors: Y. Wu, M. Arif Mohamed, Martin Skote
Simulations via computational fluid dynamics (CFD) have offered various insights into the flow physics of rotational aerodynamics.
However, CFD over such flows is not a straight-forward case.
While the computations of direct numerical simulations (DNS) are highly sought after, they are not realistically feasible due to the high computational overheads.
Based on this, the simulations were set to a steady state full rotation of the blade.
Sørensen, Aerofoil characteristics from 3D CFD rotor computations.
However, CFD over such flows is not a straight-forward case.
While the computations of direct numerical simulations (DNS) are highly sought after, they are not realistically feasible due to the high computational overheads.
Based on this, the simulations were set to a steady state full rotation of the blade.
Sørensen, Aerofoil characteristics from 3D CFD rotor computations.
Online since: June 2014
Authors: Nor Azwadi Che Sidik, Aman Ali Khan
In the late two decades, the LBM has advanced to such an extent that it has become a versatile and competitive alternative for Computational Fluid Dynamics (CFD) in many areas [2].
The advantages of LBM compare with conventional CFD method were LBM is simple calculation procedure; it is efficient implementation for parallel computation, easy and robust handling of complex geometry and others [4].
There are various numerical simulation have been done using different thermal LB model to investigate natural convection based on their advantages of LBM [5, 6].
Shan, Simulation of Raylaigh-Bernard convection using a lattice Boltzmann method, Phys Rev E 55 (1997) 2780-2788
In Rarefied Gas Dynamics: Theory and Simulations, Progr Astronaut Aero 159 (1992) 450-458
The advantages of LBM compare with conventional CFD method were LBM is simple calculation procedure; it is efficient implementation for parallel computation, easy and robust handling of complex geometry and others [4].
There are various numerical simulation have been done using different thermal LB model to investigate natural convection based on their advantages of LBM [5, 6].
Shan, Simulation of Raylaigh-Bernard convection using a lattice Boltzmann method, Phys Rev E 55 (1997) 2780-2788
In Rarefied Gas Dynamics: Theory and Simulations, Progr Astronaut Aero 159 (1992) 450-458
Online since: October 2011
Authors: Xiao Ying Hu, Ning Wang, Chang Qing Dong, Ying Zhao, Da Long Jiang, Qin Liang Tan
And fluent 6.3 has been used to perform the simulation as the solver.
Fig. 2 shows the simulation result for case 1, case 2, case 3, case 4, and case 5.
And then in Fig. 2 the last two pictures show that simulation results for case 4, case 5.
Since the flow characteristics and turbulence kinetic energy are difficult to observe, the CFD studies can be an useful tool for researching the performance in the modern life.
Zhang: CFD Studies on the air flow in a double-grate biomass fired boiler (IEEE Computer Society, China 2010) [8] Y.B.
Fig. 2 shows the simulation result for case 1, case 2, case 3, case 4, and case 5.
And then in Fig. 2 the last two pictures show that simulation results for case 4, case 5.
Since the flow characteristics and turbulence kinetic energy are difficult to observe, the CFD studies can be an useful tool for researching the performance in the modern life.
Zhang: CFD Studies on the air flow in a double-grate biomass fired boiler (IEEE Computer Society, China 2010) [8] Y.B.
Online since: February 2013
Authors: Vahid Balouchestani Asl, Somayeh Davoudabadi Farahani
(Simulation of separation is not the purpose of this article)
Launch Vehicle Data
The pilot launch vehicle is a single-stage solid propellant rocket with 104 seconds of burning time.
Simulating Flight Path Data processing by standard three degree of freedom simulation provides flight path, pitch angles and Mach number are extracted for power-on phase.
According to flight simulation outputs, pressure distribution in different Mach numbers is obtained by using FLUENT software CFD simulation.
Assumptions used for the simulation is as follows: To achieve more accurate results in performed simulations, the k-ε-RNG turbulence model is used.
In the simulation, the density is calculated using the ideal gas law.
Simulating Flight Path Data processing by standard three degree of freedom simulation provides flight path, pitch angles and Mach number are extracted for power-on phase.
According to flight simulation outputs, pressure distribution in different Mach numbers is obtained by using FLUENT software CFD simulation.
Assumptions used for the simulation is as follows: To achieve more accurate results in performed simulations, the k-ε-RNG turbulence model is used.
In the simulation, the density is calculated using the ideal gas law.