Computation of charge and ion drag force on multiple static spherical dust grains immersed in rf discharges

2010 ◽  
Vol 17 (10) ◽  
pp. 103712 ◽  
Author(s):  
V. R. Ikkurthi ◽  
K. Matyash ◽  
A. Melzer ◽  
R. Schneider
Keyword(s):  
2000 ◽  
pp. 531-534
Author(s):  
Shigehiko Nonaka ◽  
Kouji Katoh ◽  
Yoshiharu Nakamura ◽  
Shunjiro Ikezawa ◽  
Shuichi Takamura
Keyword(s):  

2004 ◽  
Vol 202 ◽  
pp. 375-377
Author(s):  
Taku Takeuchi ◽  
Pawel Artymowicz

In optically thin gas disks around young Vega-type stars, dust grains are exposed to the stellar radiation pressure and gas drag force. The combination of these forces pushes the grains away from the central star. Typically, 10–100 μm grains migrate outward to become concentrated at the outer edge of the gas disk. A dust ring naturally forms without the help of clearing bodies, such as planets or brown dwarfs.


2009 ◽  
Vol 16 (4) ◽  
pp. 043703 ◽  
Author(s):  
V. R. Ikkurthi ◽  
K. Matyash ◽  
A. Melzer ◽  
R. Schneider
Keyword(s):  

2009 ◽  
Vol 390-391 ◽  
pp. 103-105 ◽  
Author(s):  
K. Matyash ◽  
R. Schneider ◽  
V.R. Ikkurthi ◽  
A. Melzer
Keyword(s):  

2020 ◽  
Vol 22 (4) ◽  
pp. 1047-1060
Author(s):  
S. Shadmani ◽  
S. M. Mousavi Nainiyan ◽  
R. Ghasemiasl ◽  
M. Mirzaei ◽  
S. G. Pouryoussefi

AbstractAhmed Body is a standard and simplified shape of a road vehicle that's rear part has an important role in flow structure and it's drag force. In this paper flow control around the Ahmed body with the rear slant angle of 25° studied by using the plasma actuator system situated in middle of the rear slant surface. Experiments conducted in a wind tunnel in two free stream velocities of U = 10m/s and U = 20m/s using steady and unsteady excitations. Pressure distribution and total drag force were measured and smoke flow visualization carried out in this study. The results showed that at U = 10m/s using plasma actuator suppress the separated flow over the rear slant slightly and be effective on pressure distribution. Also, total drag force reduces in steady and unsteady excitations for 3.65% and 2.44%, respectively. At U = 20m/s, using plasma actuator had no serious effect on the pressure distribution and total drag force.


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