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Transverse Pressure

Equilibration of the interface, and the establislnnent of equilibrium between the two phases, may be very slow. Holcomb et al [183] found that the density profile p(z) equilibrated much more quickly than tire profiles of nonnal and transverse pressure, f yy(z) and f jfz), respectively. The surface tension is proportional to the z-integral of Pj z)-Pj z). The bulk liquid in the slab may continue to contribute to this integral, indicatmg lack of equilibrium, for very long times if the initial liquid density is chosen a little too high or too low. A recent example of this kind of study, is the MD simulation of the liquid-vapour surface of water at temperatures between 316 and 573 K by Alejandre et al [184]. [Pg.2271]

Flow diversions that occur due to imposed transverse pressure gradients... [Pg.475]

Figure 10. Time History of Net Transverse Pressure on Object during Passage of a Blast Wave. Figure 10. Time History of Net Transverse Pressure on Object during Passage of a Blast Wave.
Profiles are all extruded articles having a cross-sectional shape that differs from that of a circle, an annulus, or a very wide and thin rectangle (flat film or sheet). The cross-sectional shapes are usually complex, which, in terms of solving the flow problem in profile dies, means complex boundary conditions. Furthermore, profile dies are of nonuniform thickness, raising the possibility of transverse pressure drops and velocity components, and making the prediction of extrudate swelling for viscoelastic fluids very difficult. For these reasons, profile dies are built today on a trial-and-error basis, and final product shape is achieved with sizing devices that act on the extrudate after it leaves the profile die. [Pg.731]

Figure 10 presents the interface shape of the rivulet for wall superheat as 0.5 K and Re = 2.5. Here also presented the data on pressure in liquid and heat flux density in rivulet cross-section. The intensive liquid evaporation in near contact line region causes the interface deformation. As a result the transversal pressure gradient creates the capillarity induced liquid cross flow in direction to contact line. Finally the balance of evaporated liquid and been bring by capillarity is established. This balance defines the interface shape and apparent contact angle value.For the inertia flow model, the solution is obtained from a non-stationary system of equations, i.e., it is time-dependable. In this case the disturbances in flow interface can create the wave flow patterns. The solutions of unsteady state liquid spreading on heat transfer surface without and with evaporation are presented on Fig. 11. When the evaporation is not included (for zero wall superheat) the wave pattern appears on the interface. When the evaporation includes, the apparent contact angle increase immediately and deform the interface. It causes the wave suppression due to increasing of the film curvature. Figure 10 presents the interface shape of the rivulet for wall superheat as 0.5 K and Re = 2.5. Here also presented the data on pressure in liquid and heat flux density in rivulet cross-section. The intensive liquid evaporation in near contact line region causes the interface deformation. As a result the transversal pressure gradient creates the capillarity induced liquid cross flow in direction to contact line. Finally the balance of evaporated liquid and been bring by capillarity is established. This balance defines the interface shape and apparent contact angle value.For the inertia flow model, the solution is obtained from a non-stationary system of equations, i.e., it is time-dependable. In this case the disturbances in flow interface can create the wave flow patterns. The solutions of unsteady state liquid spreading on heat transfer surface without and with evaporation are presented on Fig. 11. When the evaporation is not included (for zero wall superheat) the wave pattern appears on the interface. When the evaporation includes, the apparent contact angle increase immediately and deform the interface. It causes the wave suppression due to increasing of the film curvature.
The presence of an isotropic ferroelectric transition is also reflected by the total configm-ational potential energy per particle U /N plotted in the inset of Fig. 6.6. Increasing P from the initial smaller values, U) /N first increases, but then begins to decrease at a transverse pressure of about 7 11 2.0 where Pi begins to rise rather sharply. Clearly, the decrease of (/) /N can only be caused by the dipolar interactions, because the short-range fluid fluid and the fluid substrate potentials are purely repulsive. [Pg.328]

The transverse pressure difference was directly demonstrated by Pieranski and Guyon< by measuring the liquid level difference in tubes connected to holes facing each other across the width / of the cell. Its dependence on predicted by (3.6.25) was verified (fig. 3.6.9(a)). It vanishes for = 0 and njl. Further, it was confirmed that it changes sign when the flow is reversed or when the field is rotated so that (j> becomes —... [Pg.158]

We note that while the longitudinal pressure is a constant, independent of z, as required by mechanical equilibrium, the transverse pressure does depend on z. In the limiting case of an isotropic system with no dependence of 71 (z) on z), Ht = = Tn 0) we recover the ideal gas law. [Pg.167]

In Ref. 4, it is shown that the bending moduli scale with the cube of the thickness of the solid thin film. A similar result can be obtained from the general discussion in this chapter, since the modulii scale with the integral of the second moment of the transverse pressure profile. However, in a solid, thin film, the possibility for incoherent bending of the layers also exists —... [Pg.208]

One of the problems with balancing by land length is that it induces transverse pressure differences along the length of the flow channel. Pressure differences across the channel will create cross flow, and this will make the effect of balancing by land length unpredictable unless a three-dimensional flow analysis is used. One way to avoid cross flow is to place partitions between the sections with different thickness of the die so that cross flow between the different sections is not possible. In effect, this creates separate die flow channels an example is shown in Fig. 9.4. [Pg.657]

The authors micro ehl solution technique derives from their earlier solution method for heavily-loaded spherical contacts (3) and the elongated elliptical contacts found in high conformity gears of the Wildhaber-Novlkov type (4), (5). The solution method, which utilises the inverse solution of the Reynolds equation, is as described in the above publications except that the elastic deformation calculation must take account of the deformation produced by pressures acting on adjacent asperities, as mentioned above, and in the solution of the lubrication equations the side boundary condition is one of zero transverse pressure gradient rather than zero pressure. [Pg.241]

A uniformly stretched rubber membrane is similar in many respects to a soap film, or the interface between two fluids. It has a uniform tension and the thickness of the membrane is small compared with the dimensions of the surface area. The analysis of section 5.2, which derives the Laplace-Young equation for a fluid interface or soap film, applies equally to a uniformly stretched membrane with a transverse pressure load that is perpendicular to the surface. So the Laplace-Young equation for the membrane is... [Pg.179]


See other pages where Transverse Pressure is mentioned: [Pg.112]    [Pg.15]    [Pg.48]    [Pg.66]    [Pg.262]    [Pg.57]    [Pg.107]    [Pg.328]    [Pg.42]    [Pg.92]    [Pg.157]    [Pg.157]    [Pg.158]    [Pg.963]    [Pg.163]    [Pg.166]    [Pg.193]    [Pg.194]    [Pg.196]    [Pg.196]    [Pg.512]    [Pg.280]    [Pg.207]    [Pg.196]    [Pg.196]    [Pg.341]    [Pg.436]    [Pg.436]    [Pg.542]    [Pg.543]    [Pg.180]    [Pg.200]   


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