2005
DOI: 10.2514/1.13530
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Capturing the Knudsen Layer in Continuum-Fluid Models of Nonequilibrium Gas Flows

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Cited by 99 publications
(82 citation statements)
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“…This concept is similar to the 'wall-function' proposed in Lockerby et al (2005b). However, there are some marked differences in the model we propose below, most notably the presence of a second-order contribution to the near-wall scaling (secondorder, in that it is dependent on a local Knudsen number) and a more accurate functional form (we also do not continue to use the phrase 'wall-function' in the present paper, to avoid confusion with those wall-functions associated with turbulence modelling).…”
Section: Near-wall Scaling Of the Constitutive Relationsmentioning
confidence: 92%
See 1 more Smart Citation
“…This concept is similar to the 'wall-function' proposed in Lockerby et al (2005b). However, there are some marked differences in the model we propose below, most notably the presence of a second-order contribution to the near-wall scaling (secondorder, in that it is dependent on a local Knudsen number) and a more accurate functional form (we also do not continue to use the phrase 'wall-function' in the present paper, to avoid confusion with those wall-functions associated with turbulence modelling).…”
Section: Near-wall Scaling Of the Constitutive Relationsmentioning
confidence: 92%
“…The functional form given in (24) is qualitatively different to that proposed by Lockerby et al (2005b) and Guo et al (2007), and has been chosen to reproduce the Knudsen layer's actual structure more accurately; it allows for an indefinitely steep profile in the inner most regions of the Knudsen layer, and a more gradual decay in the outer regions. It also allows for a second-order contribution to the Knudsen layer.…”
Section: Near-wall Scaling Of the Constitutive Relationsmentioning
confidence: 99%
“…(1.1), a low-speed micro gas flow will have a uniformly negligible local Knudsen number because the gradients of the flow variables are negligibly small. Nevertheless, non-equilibrium effects are far from negligible in these cases (Lockerby et al 2005a). For hypersonic aerodynamic flows it has been suggested (Macrossan 2006) that Ma · Kn L , where Ma is the local Mach number, is a more appropriate breakdown parameter; however, this parameter would be inappropriate for low-speed gas flows, which have a very small Mach number but can still be quite rarefied.…”
Section: Introductionmentioning
confidence: 99%
“…Instead, the technique we investigate in this paper is the method of constitutiverelation scaling developed by Lockerby et al [2]. This technique uses linearised kinetic theory results to determine a phenomenological function f (n/λ) with which to scale the constitutive relationship for shear stress in planar flows, i.e.…”
Section: Constitutive-relation Scalingmentioning
confidence: 99%
“…The slip coefficient ζ slip , equal to 1 in Maxwell's original derivation, is taken to be ≈ 0.8 when constitutive-relation scaling methods are used (as described below) because this value better approximates the true slip magnitude for gas flow over planar surfaces [2]. For temperature jump at solid boundaries, Smoluchowski's description is used [3]:…”
mentioning
confidence: 99%