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Local shearing stress coefficient

The conventional dimensionless measure of the local shear stress (the friction coefficient) is... [Pg.501]

The modeling procedure can be sketched as follows. First an approximate description of the velocity distribution in the turbulent boundary layer is required. The universal velocity profile called the Law of the wall is normally used. The local shear stress in the boundary layer is expressed in terms of the shear stress at the wall. From this relation a dimensionless velocity profile is derived. Secondly, a similar strategy can be used for heat and species mass relating the local boundary layer fluxes to the corresponding wall fluxes. From these relations dimensionless profiles for temperature and species concentration are derived. At this point the concentration and temperature distributions are not known. Therefore, based on the similarity hypothesis we assume that the functional form of the dimensionless fluxes are similar, so the heat and species concentration fluxes can be expressed in terms of the momentum transport coefficients and velocity scales. Finally, a comparison of the resulting boundary layer fluxes with the definitions of the heat and mass transfer coefficients, indiates that parameterizations for the engineering transfer coefficients can be put up in terms of the appropriate dimensionless groups. [Pg.625]

CNT can markedly reinforce polystyrene rod and epoxy thin film by forming CNT/polystyrene (PS) and CNT/epoxy composites (Wong et al., 2003). Molecular mechanics simulations and elasticity calculations clearly showed that, in the absence of chemical bonding between CNT and the matrix, the non-covalent bond interactions including electrostatic and van der Waals forces result in CNT-polymer interfacial shear stress (at OK) of about 138 and 186MPa, respectively, for CNT/ epoxy and CNT/PS, which are about an order of magnitude higher than microfiber-reinforced composites, the reason should attribute to intimate contact between the two solid phases at the molecular scale. Local non-uniformity of CNTs and mismatch of the coefficients of thermal expansions between CNT and polymer matrix may also promote the stress transfer between CNTs and polymer matrix. [Pg.193]

Although Ey and are analogous to fj. and v, respectively, in that all these quantities are coefficients relating shear stress and velocity gradient, there is a basic difference between the two kinds of quantities. The viscosities n and v are true properties of the fluid and are the macroscopic result of averaging motions and momenta of myriads of molecules. The eddy viscosity and the eddy diffusivity are not just properties of the fluid but depend on the fluid velocity and the geometry of the system. They are functions of all factors that influence the detailed patterns of turbulence and the deviating velocities, and they are especially sensitive to location in the turbulent field and the local values of the scale and intensity of the turbulence. Viscosities can be measured on isolated samples of fluid and presented in tables or charts of physical properties, as in Appendixes 8 and 9. Eddy viscosities and diffusivities are determined (with difficulty, and only by means of special instruments) by experiments on the flow itself. [Pg.56]

For a given value of x and the same flow properties, the boundary layer on a cone (k = 1) is thinner by a factor of 1/V3, and the surface shear stress and heat transfer are larger by a factor of V3. The local skin friction and heat transfer coefficients are related similarly ... [Pg.465]

An interfacial shear may be very important in so-called shear-controlled condensation because downward interfacial shear reduces the critical Re number for onset of turbulence. In such situations, the correlations must include interfacial shear stress, and the determination of the heat transfer coefficient follows the Nusselt-type analysis for zero interfacial shear [76], According to Butterworth [81], data and analyses involving interfacial shear stress are scarce and not comprehensive enough to cover all important circumstances. The calculations should be performed for the local heat transfer coefficient, thus involving step-by-step procedures in any condenser design. The correlations for local heat transfer coefficients are presented in [81] for cases where interfacial shear swamps any gravitational forces in the film or where both vapor shear and gravity are important. [Pg.1334]

Coulomb friction, with the shear stress being limited to a maximum value dependent on the local normal pressure. Because Coulomb friction depends on the normal stress, this is only valid for hnite element analysis in which the elasticity is included. It is most commonly applied to model the shoulder contact but requires the assumption of a constant coefficient of friction, usually calibrated via the net measured torque or indirectly through the temperature held, which reflects the fric-honal heat input. [Pg.200]

Obtain expressions for the local and mean values of the wall shear stress and friction factor (or drag coefficient) for the laminar boundary layer flow of an incompressible power-law fluid over a flat plate Compare these results with the predictions presented in Table 7.1 for different values of the power-law index. [Pg.418]

Micro- and Nanoscale Anemometry Implication for Biomedical Applications, Fig. 8 (a) An array of MEMS sensors embedded in a 3D bifurcation model, (b) Computational fluid dynamics (CFD) solutions for skin friction coefficient (Cf) at a Reynolds number of 6.7. Cf represents local wall shear stress values normalized by the... [Pg.1785]

Micro- and Nanoscale Anemometry Implication for Biomedical AppiicaUens, Rgure 8 (a) An array of MEMS sensors embedded in a 3D bifurcation model, (b) Computational fluid dynamics (CFD) solutions for skin friction coefficient (Cf) at a R nolds number of 6.7. Cj represents local wall shear stress values normalized by the upstream dynamic pressure. Cj values are shown along the interior surface of bifurcation, (c) Comparison of the CFD On blue), experimental On green), and theoretical On red) skin friction for the 180° edge. x/D/cos(12.5) is the x distance normalized to the diameter of the inlet pipe and parallel to the centerline of the outlet pipes... [Pg.1279]

The mixed film pressure distribution is used to evaluate the corresponding contact deformed geometry, the lubricant film shear stresses, the lubricant and surfaces temperatures and the contact friction coefficient. The model admits the non-Newtonian behaviour of the lubricant and a local distribution of the temperature inside the contact. It was used to predict the friction coefficient along the meshing line of a FZG type C gear. [Pg.603]

Figure 9 shows the lubricant film shear stress field, t(x), and local friction coefficient /j(x), calculated in at same point of the gear meshing line (point A) and for the same operating conditions. The global friction coefficient at point A (/UgA) is about 0.03. [Pg.608]

Instead of carrying out equilibrium averaging, one can introduce a consistently averaged hydro-dynamic interaction , in which the averaging is not performed with the equilibrium distribution function, but rather with a distribution function that is consistent with the local flow field.This leads to shear-rate dependence for all the viscometric functions, and also to a nonzero (but positive) value of the second normal stress coefficient. [Pg.257]

Simple shear, in which u = u y, with u, T, and v constants, is exceptional. It occurs when the diameter and solid volume fraction of the flow spheres, the diameter and separation of the wall hemispheres, and the two coefficients of restitution are such that in the interior and at the boundaries, the rate at which fluctuation energy is produced by the shear stress working through the mean velocity gradient or through the slip velocity is precisely equal to the local rate at which it is dissipated in collisions. We first treat this homogeneous flow, noting that the apparent rate of shear 2U/L differs from u by 2v/L because of slip at the boundary. [Pg.165]


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See also in sourсe #XX -- [ Pg.257 ]




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