2005
DOI: 10.1063/1.1868034
|View full text |Cite
|
Sign up to set email alerts
|

Inverted velocity profiles in rarefied cylindrical Couette gas flow and the impact of the accommodation coefficient

Abstract: Cylindrical Couette gas flow in the noncontinuum regime has been investigated using the boundary treatment derived from Maxwell's slip-flow model. It is shown that the tangential momentum accommodation coefficient plays an important role in determining the predicted velocity profile. The present analysis is in close agreement with previous analytical studies and shows good qualitative agreement with available direct simulation Monte Carlo data. The results predict the presence of an inverted velocity profile f… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
2
1

Citation Types

2
32
1

Year Published

2006
2006
2015
2015

Publication Types

Select...
7
1

Relationship

2
6

Authors

Journals

citations
Cited by 57 publications
(35 citation statements)
references
References 14 publications
2
32
1
Order By: Relevance
“…It is clear that at Kn= 0.5, the analytical slip-flow solution cannot be relied upon and this discrepancy clearly grows with increasing oscillatory frequency. Although it is recognized that this is well beyond the accepted limit of the slip-flow regime, the results presented indicate a significant difference to the steady-state case ͑␤ → 0͒ where several authors 25,28 have shown good agreement between analytical solutions and DSMC data for Kn= 0.5 and Mach numbers up to 0.5.…”
Section: Results For the Transition Regimecontrasting
confidence: 62%
See 2 more Smart Citations
“…It is clear that at Kn= 0.5, the analytical slip-flow solution cannot be relied upon and this discrepancy clearly grows with increasing oscillatory frequency. Although it is recognized that this is well beyond the accepted limit of the slip-flow regime, the results presented indicate a significant difference to the steady-state case ͑␤ → 0͒ where several authors 25,28 have shown good agreement between analytical solutions and DSMC data for Kn= 0.5 and Mach numbers up to 0.5.…”
Section: Results For the Transition Regimecontrasting
confidence: 62%
“…However, the shear stress associated with the outer cylinder increases away from the oscillating wall at low frequencies, as indicated for the case of ␤ = 1 and for the limiting case of ␤ = 0, which is equivalent to the steady rotating Couette problem. 28 At first glance this may appear unusual, but it is due to the requirement that the torque on each cylinder must balance. It is straightforward to show that in the limit of ␤ → 0, the shear stress on the inner cylinder will approach ͑r 2 / r 1 ͒ 2 , which, for this particular case, results in a shear stress that is four times higher on the inner cylinder.…”
Section: B Results For Nonplanar Couette Flow In the Slip Regimementioning
confidence: 96%
See 1 more Smart Citation
“…The fluid particles and the wall particles at a distance r interact through a LennardJones(LJ) potential, V ij (r) = 4ǫ[(r/σ) −12 − A ij (r/σ) −6 ], where ǫ and σ represent the energy and length scales, and A ij = A ji is a dimensionless parameter that controls the attractive part of the potential for the fluid-fluid and the fluid-wall particles. As mentioned previously, this parameter is similar to the accommodation coefficient in continuum descriptions [1,2,3,4,5,6]. The potential is truncated at r c = 2.5σ.…”
Section: Molecular Dynamics Simulationsmentioning
confidence: 98%
“…Reliable tools exist for the prediction of gas damping in the first two regimes (see e.g. [7][8][9][10][11][12][13]46]) but the situation is less defined at lower pressures. Even though numerical techniques of deterministic and statistical nature have been developed in the transition regime (see e.g.…”
Section: Introductionmentioning
confidence: 99%