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Online since: June 2016
Authors: Anh Tuan Phan
A Study on Hovercraft Resistance Using Numerical Modeling
Phan Anh Tuan
Full Hanoi University of Science and Technology
No.1 Daicoviet road, Hanoi, Vietnam
Email: tuan.phananh@hust.edu.vn
Keywords: Hovercraft resistance, Minimizing fuel consumption, CFD.
This paper presents a method for calculating hovercraft resistance using computational fluid dynamics (CFD) tools.
This paper presents a method for calculating hovercraft resistance using computational fluid dynamics (CFD) tools.
Computational domain for CFD simulation in this study is showing in Fig.3.
Figure 2 3D model of hovercraft Figure 3 Domain for CFD Result and Discussion Velocity and pressure distribution.
This paper presents a method for calculating hovercraft resistance using computational fluid dynamics (CFD) tools.
This paper presents a method for calculating hovercraft resistance using computational fluid dynamics (CFD) tools.
Computational domain for CFD simulation in this study is showing in Fig.3.
Figure 2 3D model of hovercraft Figure 3 Domain for CFD Result and Discussion Velocity and pressure distribution.
Online since: October 2014
Authors: Xiao Han Cheng, Shan Ming Luo, Xue Feng Chang, Dan Xie
ICEM CFD is used in this paper to mesh the model.
(18) CFD Simulation Results Without Wings.
NUMERICAL SIMULATION STUDY OF GROUND EFFECTS ON FLOW FIELDAROUND VEHICLE BODIES, J.
Proficient in CFD Engineering Simulation and Case Combat—FLUENT GAMBIT ICEM CFD Tecplot, M.
CFD Simulation and Experimental Study on the Aerodynamic Characteristics of a F1 Racing Car, J.
(18) CFD Simulation Results Without Wings.
NUMERICAL SIMULATION STUDY OF GROUND EFFECTS ON FLOW FIELDAROUND VEHICLE BODIES, J.
Proficient in CFD Engineering Simulation and Case Combat—FLUENT GAMBIT ICEM CFD Tecplot, M.
CFD Simulation and Experimental Study on the Aerodynamic Characteristics of a F1 Racing Car, J.
Online since: October 2015
Authors: Thananchai Leephakpreeda, Natapol Korprasertsak
This study presents optimal design of wind booster, by utilizing Computational Fluid Dynamics (CFD).
In CFD-based experiments, guiding and throttling effects of the wind booster are able to increase mechanical power of a VAWT.
In this work, a wind booster is proposed for CFD-based analysis and optimization in order to improve angular speed of the VAWTs.
Results and discussion The experiments of VAWT rotations are performed with CFD-based simulations by utilizing XFlowTM CFD software [5].
In simulations, the wind speed is varied from 1 m/s to 8 m/s for low wind speed conditions.
In CFD-based experiments, guiding and throttling effects of the wind booster are able to increase mechanical power of a VAWT.
In this work, a wind booster is proposed for CFD-based analysis and optimization in order to improve angular speed of the VAWTs.
Results and discussion The experiments of VAWT rotations are performed with CFD-based simulations by utilizing XFlowTM CFD software [5].
In simulations, the wind speed is varied from 1 m/s to 8 m/s for low wind speed conditions.
Online since: August 2010
Authors: Ying Chao Zhang, Zhe Zhang, Jie Li
Recently a few papers mentioned the numerical simulations based CFD to study the aerodynamic
characteristic of the two vehicles crossing each other.
Recent some numerical simulations were carried out.
One commercial CFD software--STAR-CD provides with the functions.The domain and boundary setting are showed in Fig.1.
At first the single car and coach are simulations by CFD separatedly.
Comparing with the all the vehicle model results from CFD and test, little difference is found.
Recent some numerical simulations were carried out.
One commercial CFD software--STAR-CD provides with the functions.The domain and boundary setting are showed in Fig.1.
At first the single car and coach are simulations by CFD separatedly.
Comparing with the all the vehicle model results from CFD and test, little difference is found.
Online since: January 2014
Authors: De Hui Liu, Gang Tang, Li Wen Liu, Hong Min Wen, Ming Xiang Xie, Quan Guo Lu
Meanwhile, the finite model of the valveless micropump is built by using the ANSYS/FLOTRAN CFD finite element software, and coupled-field simulation analysis is carried out.
Finite Element Simulation It is an effective way to design micropump with the finite element simulation.
We have used ANSYS/FLOTRAN CFD software for the simulation of the fluid in micropump, including two-dimensional and three-dimensional simulation.
A fluid element, FLUID142, is used in three-dimensional simulation, while FLUID 141 in two-dimensional simulation.
Fig.9 The pressure contour of micro pump Fig.10 The pressure distribution of diffusion/shrinkage tube Conclusion Based on the flow property of diffusion and shrinkage elements, the theory analysis is developed for a valveless micropump, and the finite model of the valveless micropump is built by using the ANSYS/FLOTRAN CFD finite element software, and coupled-field simulation analysis is carried out.
Finite Element Simulation It is an effective way to design micropump with the finite element simulation.
We have used ANSYS/FLOTRAN CFD software for the simulation of the fluid in micropump, including two-dimensional and three-dimensional simulation.
A fluid element, FLUID142, is used in three-dimensional simulation, while FLUID 141 in two-dimensional simulation.
Fig.9 The pressure contour of micro pump Fig.10 The pressure distribution of diffusion/shrinkage tube Conclusion Based on the flow property of diffusion and shrinkage elements, the theory analysis is developed for a valveless micropump, and the finite model of the valveless micropump is built by using the ANSYS/FLOTRAN CFD finite element software, and coupled-field simulation analysis is carried out.
Online since: January 2019
Authors: F. Mechighel, S. Ben Aoua, S. Dost
The lattice Boltzmann method (LBM) is relatively novel and contrasts with the usual well-known methods to physical modeling in the domain of computational fluid dynamics (CFD).
Indeed two different matters with special ingredients and ideas are handled when the LBM is considered to physical modeling in the CFD domain instead of the usual numerical methods.
Dimensionless parameters used in the simulation and their characteristic values, calculated for SiGe solution, are predicted from [47].
The present LBE-based model is found numerically more efficient than usual CFD methods under particular situations.
[27] Swift, M.R.; Orlandi, E.; Osborn, W.R.; Yeomans, J.M. (1996): Lattice Boltzmann simulations of liquid–gas and binary fluid systems.
Indeed two different matters with special ingredients and ideas are handled when the LBM is considered to physical modeling in the CFD domain instead of the usual numerical methods.
Dimensionless parameters used in the simulation and their characteristic values, calculated for SiGe solution, are predicted from [47].
The present LBE-based model is found numerically more efficient than usual CFD methods under particular situations.
[27] Swift, M.R.; Orlandi, E.; Osborn, W.R.; Yeomans, J.M. (1996): Lattice Boltzmann simulations of liquid–gas and binary fluid systems.
Online since: January 2015
Authors: Wei Liu, Yun Fei Zhao, Xu Liu
Finally, the unsteady flow field of a reduced order model development trends and application prospect were analyzed, and pointing out that the CFD simulation is still accurately predict the plane stability and handling the most important method.
In addition, the scope of application of reduced-order model is currently mostly other simple shape of the wing subsonic, transonic simulation, simulation of supersonic complex shape to be further developed.
Therefore, CFD method is still accurate prediction of aircraft stability and handling of the most important methods.
NonlinearDynamicsAnalysisofrMechanism of slender WIng Rock and study of Numerical Simulation Method [D].
Aircraft multi degree of freedom coupling rock movement numerical simulation research [D].
In addition, the scope of application of reduced-order model is currently mostly other simple shape of the wing subsonic, transonic simulation, simulation of supersonic complex shape to be further developed.
Therefore, CFD method is still accurate prediction of aircraft stability and handling of the most important methods.
NonlinearDynamicsAnalysisofrMechanism of slender WIng Rock and study of Numerical Simulation Method [D].
Aircraft multi degree of freedom coupling rock movement numerical simulation research [D].
Online since: December 2012
Authors: Feng Jin
In order to study the specialties of wave slamming on open-piled structures, a two-dimensional regular wave tank was established based on commercial CFD software FLUENT.
In the following sections, the two-dimensional regular wave tank was established based on commercial CFD software FLUENT.
Table 1 shows the comparison results of simulation and the experiment.
Numerical Simulation of Random Wave Slamming on Structures in the Splash Zone.
Prediction of Wave-in-deck Forces on Fixed Jacket-type Structures Based on CFD Calculations.
In the following sections, the two-dimensional regular wave tank was established based on commercial CFD software FLUENT.
Table 1 shows the comparison results of simulation and the experiment.
Numerical Simulation of Random Wave Slamming on Structures in the Splash Zone.
Prediction of Wave-in-deck Forces on Fixed Jacket-type Structures Based on CFD Calculations.
Online since: October 2011
Authors: Da Hua Jiang, An Gui Li, Fa En Shi, Zhi Hua Wang
This article uses CFD to study the efficiency of ventilation and pollution discharge of double polluted sources in the lab, and investigate the effect of air exhaust outlet location and air supply velocity on the performance of side ventilation.
CFD is one kind of rapidly developing computer aided design technology in recent years, CFD can be effective airflow organization simulation on indoor ventilation and air conditioning design before equipment installation.
This article explores effective ventilation method of double gaseous polluted Sources at side ventilation type by CFD.
H, room height), simulation is done at the air supply velocity of 0.4m/s,0.6m/s, 0.8m/s,1.0m/s,temperature field and velocity field is simplified as non-dimension at work area (y=3.5m,x=3m,z=0.1-1.8m).
Perceived air quality, sick building syndrome (SBS) ,symptoms and product ivity in an of office with two different pollution loads [J].Indoor Air,1999,(9):165-179 [4] Xianting Li,Bin Zhao.Numerical Simulation of Indoor Airflow[M].Beijing: Mechanical industry press,2009.in chinese
CFD is one kind of rapidly developing computer aided design technology in recent years, CFD can be effective airflow organization simulation on indoor ventilation and air conditioning design before equipment installation.
This article explores effective ventilation method of double gaseous polluted Sources at side ventilation type by CFD.
H, room height), simulation is done at the air supply velocity of 0.4m/s,0.6m/s, 0.8m/s,1.0m/s,temperature field and velocity field is simplified as non-dimension at work area (y=3.5m,x=3m,z=0.1-1.8m).
Perceived air quality, sick building syndrome (SBS) ,symptoms and product ivity in an of office with two different pollution loads [J].Indoor Air,1999,(9):165-179 [4] Xianting Li,Bin Zhao.Numerical Simulation of Indoor Airflow[M].Beijing: Mechanical industry press,2009.in chinese
Comparative Studies on Various Turbulent Models with Liquid Rocket Nozzle through Computational Tool
Online since: July 2014
Authors: N.K. Mohamad Tanveer, Chandran Mohanraj, K. Jegadeesan, S. Maruthupandiyan
Introduction
Computational Fluid Dynamics (CFD) is an engineering tool that assists experimentation.
Its scope is not limited to fluid dynamics; CFD could be applied to any process which involves transport phenomena with it.
In CFD a problem is simulated in software and the transport equations associated with the problem is mathematically solved with computer assistance.
The turbulent dynamic viscosity is computed from μt = ρν ∱ν1 (6) K- Model The standard K- model was considered for this simulation.
Bartosiewicz, Zine Aidoun, “CFD-Experiments Integration in the Evaluation of Six Turbulence Models for Supersonic Ejectors Modeling” CETC-Varennes, Natural Ressources Canada, ybartosi@RNCan.gc.ca [8]C.Mohanraj, Dr.P.K.Srividhya, “CFD Simulation of 20 kW Downdraft Gasifier” International Journal of Current Engineering and Technology ISSN 2277 - 4106, Vol.3, No.1 (March 2013) [9] K.M.
Its scope is not limited to fluid dynamics; CFD could be applied to any process which involves transport phenomena with it.
In CFD a problem is simulated in software and the transport equations associated with the problem is mathematically solved with computer assistance.
The turbulent dynamic viscosity is computed from μt = ρν ∱ν1 (6) K- Model The standard K- model was considered for this simulation.
Bartosiewicz, Zine Aidoun, “CFD-Experiments Integration in the Evaluation of Six Turbulence Models for Supersonic Ejectors Modeling” CETC-Varennes, Natural Ressources Canada, ybartosi@RNCan.gc.ca [8]C.Mohanraj, Dr.P.K.Srividhya, “CFD Simulation of 20 kW Downdraft Gasifier” International Journal of Current Engineering and Technology ISSN 2277 - 4106, Vol.3, No.1 (March 2013) [9] K.M.