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Online since: October 2011
Authors: Zhi Qiang Huang, Zhen Chen, Rong Gai Zhu, Xue Yuan Li, Shuang Jing, Jing Wang, Xing Huang
Stimulation Analyses
With application of computational fluid dynamics (CFD) software Fluent [10], the flow pattern of natural gas transporting in the pipeline has been simulated before and after DRA injected, with purpose of revealing the gas flow pattern’s improvement law of DRA acted on the internal wall of pipeline.
FLUNENT: Computer Simulation of Fluid Engineering and Application Examples[M].
FLUNENT: Computer Simulation of Fluid Engineering and Application Examples[M].
Online since: April 2016
Authors: Thomas Panten, Heiko Meironke
With the help of numerical simulations can be nowadays flows represent very detailed and accurate.
Due to the strongly three dimensional and unsteady turbulent characteristics of flow, which are marked with vortex shedding, flow reattachment and recirculation bubbles, the CFD reaches its limits.
Due to the strongly three dimensional and unsteady turbulent characteristics of flow, which are marked with vortex shedding, flow reattachment and recirculation bubbles, the CFD reaches its limits.
Online since: November 2011
Authors: Neng Zhu, Zhe Tian, Yan Ding
Because CFD (Computational Fluid Dynamics) embraces the advantages of visualization and economy, it has become the main method to study the dispersion routes of indoor particles.
However, nearly all experimental validations for computational simulation choose gaseous pollutants or dust particles as research objects, while pertinent bio-aerosols are hardly used.
However, nearly all experimental validations for computational simulation choose gaseous pollutants or dust particles as research objects, while pertinent bio-aerosols are hardly used.
Online since: September 2008
Authors: Christian Boller, Chen Mig Kuo, Ning Qin
Along some FSI simulation performed for the reference design shown in Fig.
5 it has been shown, that even for wings with a small span the deflection as shown in Fig. 7 (left)
can be remarkable.
Numeric validation performed has been based on a major simulation environment consisting of CAD, CFD and FE software.
Simulations were performed for a variety of flight conditions and parameters.
What those results show as well as a variety of other simulation Time [sec] W Time [sec] W Fully extracted wing Half extracted wing Fully contracted wing 0 -0.05 -0.1 -0.15 0.05 Time [sec] W Time [sec] W Time [sec] W Time [sec] W Fully extracted wing Half extracted wing Fully contracted wing 0 -0.05 -0.1 -0.15 0.05Inverse Zimmerman Original Zimmerman Inverse Zimmerman Original Zimmerman 0 5 10 15 20 25 30 35 -6 -4 -2 0 2 4 6 8 10 Time [sec] Change in U velocity [m/sec] Rigid wing MAV Flexible wing MAV 0 5 10 15 20 25 30 35 -6 -4 -2 0 2 4 6 8 10 Time [sec] Change in U velocity [m/sec] Rigid wing MAV Flexible wing MAV Rigid wing MAV Flexible wing MAV Individual Spar Rotation Angle Individual Spar Rotation Angle results described in [3] show is that the flexible MAV wing provides better stability compared to a rigid MAV wing.
To compare the performance between a conventional MAV steered by a rudder and the vector thrust steered alternative an analytic simulation model has been applied which has been described in further detail in [3].
Numeric validation performed has been based on a major simulation environment consisting of CAD, CFD and FE software.
Simulations were performed for a variety of flight conditions and parameters.
What those results show as well as a variety of other simulation Time [sec] W Time [sec] W Fully extracted wing Half extracted wing Fully contracted wing 0 -0.05 -0.1 -0.15 0.05 Time [sec] W Time [sec] W Time [sec] W Time [sec] W Fully extracted wing Half extracted wing Fully contracted wing 0 -0.05 -0.1 -0.15 0.05Inverse Zimmerman Original Zimmerman Inverse Zimmerman Original Zimmerman 0 5 10 15 20 25 30 35 -6 -4 -2 0 2 4 6 8 10 Time [sec] Change in U velocity [m/sec] Rigid wing MAV Flexible wing MAV 0 5 10 15 20 25 30 35 -6 -4 -2 0 2 4 6 8 10 Time [sec] Change in U velocity [m/sec] Rigid wing MAV Flexible wing MAV Rigid wing MAV Flexible wing MAV Individual Spar Rotation Angle Individual Spar Rotation Angle results described in [3] show is that the flexible MAV wing provides better stability compared to a rigid MAV wing.
To compare the performance between a conventional MAV steered by a rudder and the vector thrust steered alternative an analytic simulation model has been applied which has been described in further detail in [3].
Online since: June 2014
Authors: Su Qin Li, Wei Wei, Hai Tao Wen, Chang Quan Zhang
Simulation of magnetic suspensions for HGMS using CFD, FEM and DEM modeling[J].
Online since: March 2020
Authors: Vitaliy Nikolaevich Schetinin, Alexander Pavlovich Sokolov, Arseniy Sergeevich Sapelkin, Konstantin Valerievich Mikhailovskiy, Mikhail Sergeevich Kuts
Simulation was made using finite element procedure.
Analysis of the effect of module design on gas absorption in cross flow hollow membrane contactors via computational fluid dynamics (CFD) analysis.
Analysis of the effect of module design on gas absorption in cross flow hollow membrane contactors via computational fluid dynamics (CFD) analysis.
Online since: January 2016
Authors: Adela Palková, Milan Palko
Program is somehow an inter-stage between simple calculations on the basis of empirical relations and modern simulation methods on the basis of CFD.
Online since: October 2025
Authors: Mohamed Bouzit, Fayçal Bouzit, Abderrahim Mokhefi, Mohammed Benyahia
Indeed, since the advent of Computational Fluid Dynamics (CFD) and the initiation of experimental work utilizing modern experimental tools, research on backward-facing steps (BFS) has gained significant momentum.
Brés and Colonius [47] performed direct numerical simulations to analyze three-dimensional instabilities in compressible flow over open cavities.
In the present simulations, the Prandtl number is set at Pr = 0.71, corresponding to air flow, while the Reynolds number is set at Re = 200.
Vengadesan, Large-eddy simulation investigation of modified rib shapes on heat transfer in a ribbed duct, J.
Chen, Numerical simulation of two-dimensional viscous flows using combined finite element-immersed boundary method, J.
Brés and Colonius [47] performed direct numerical simulations to analyze three-dimensional instabilities in compressible flow over open cavities.
In the present simulations, the Prandtl number is set at Pr = 0.71, corresponding to air flow, while the Reynolds number is set at Re = 200.
Vengadesan, Large-eddy simulation investigation of modified rib shapes on heat transfer in a ribbed duct, J.
Chen, Numerical simulation of two-dimensional viscous flows using combined finite element-immersed boundary method, J.
Online since: September 2013
Authors: Jia Ning Zhang, Yu Chen Shang, Lei Zhang
Norwegian University of Science and Technology generally through the physical model tests in ice towing tank, combined with full-scale test (if possible) and mathematical simulation methods got the approximate design load of ice ridge.
CFD calculation method has not yet been used in a real ship ice resistance calculation at present, it is the reason why this project will eventually adopt the ice model test.
CFD calculation method has not yet been used in a real ship ice resistance calculation at present, it is the reason why this project will eventually adopt the ice model test.
Online since: March 2019
Authors: Battseveen Buyankhishig, Nyamsuren Byambasuren, Enkhtuul Surenjav, Narandalai Byamba-Ochir
Bernard, Design of a reactor operating in supercritical water conditions using CFD simulations.