Assessment of the Vortex Particle-Mesh Method for Efficient LES of Hovering Rotors and their Wakes

2021 ◽  
Author(s):  
Denis-Gabriel Caprace ◽  
Grégoire Winckelmans ◽  
Philippe Chatelain
Keyword(s):  
2020 ◽  
Vol 34 (1-2) ◽  
pp. 21-48 ◽  
Author(s):  
Denis-Gabriel Caprace ◽  
Grégoire Winckelmans ◽  
Philippe Chatelain

2019 ◽  
Vol 394 ◽  
pp. 700-718 ◽  
Author(s):  
T. Gillis ◽  
Y. Marichal ◽  
G. Winckelmans ◽  
P. Chatelain

2018 ◽  
Vol 354 ◽  
pp. 692-716 ◽  
Author(s):  
Philippe Parmentier ◽  
Grégoire Winckelmans ◽  
Philippe Chatelain

2019 ◽  
Vol 61 (2) ◽  
pp. 749-762 ◽  
Author(s):  
Daniel A. White ◽  
Youngsoo Choi ◽  
Jun Kudo

2014 ◽  
Vol 69 (2) ◽  
pp. 343-356
Author(s):  
Shaohua Chen ◽  
Lauren DeDieu

Author(s):  
Guoqing Zhang ◽  
Hui Li ◽  
Shengnan Shen ◽  
Tan Trinh ◽  
Frank E. Talke ◽  
...  

The effect of track-seeking on off-track residual vibrations of the head-gimbal assembly (HGA) is investigated for air and helium environments using the so-called “fluid dynamic mesh” method and the “fluid-structure interaction” method. Three different angular acceleration profiles (square wave, triangular wave and sinusoidal wave) are investigated as a function of seek time (10 ms and 5 ms). Results show that smoothening of sharp transitions of the seek profile improves the performance of off-track residual vibrations during track-following and shortens the track-following time of the head positioning servo system. In addition, the effect of lateral flow (windage) on off-track residual vibrations during track-following must be considered for a square wave angular acceleration profile. Simulation results show that helium improves the track-following accuracy compared to air due to the lower windage forces acting on the HGA. We observe that the sinusoidal wave angular acceleration performs best among the three angular acceleration profiles investigated. Furthermore, seek time is found to have only a small effect on off-track residual vibrations during track-following.


2011 ◽  
Vol 97-98 ◽  
pp. 698-701
Author(s):  
Ming Lu Zhang ◽  
Yi Ren Yang ◽  
Li Lu ◽  
Chen Guang Fan

Large eddy simulation (LES) was made to solve the flow around two simplified CRH2 high speed trains passing by each other at the same speed base on the finite volume method and dynamic layering mesh method and three dimensional incompressible Navier-Stokes equations. Wind tunnel experimental method of resting train with relative flowing air and dynamic mesh method of moving train were compared. The results of numerical simulation show that the flow field structure around train is completely different between wind tunnel experiment and factual running. Two opposite moving couple of point source and point sink constitute the whole flow field structure during the high speed trains passing by each other. All of streamlines originate from point source (nose) and finish with the closer point sink (tail). The flow field structure around train is similar with different vehicle speed.


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