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Form incompressible fluid

Calculate This is the calculation button and must be pressed once the data entry is complete. [Pg.178]

Cancel This button is used to cancel the calculation and go back to the main form. [Pg.178]

Clear By pressing this button, all input data are cleared. This will not clear the calculated values. [Pg.178]

Roughness This help button will open a separate form for recommended pipe roughness values. These are suggested values and normally used in calculations. [Pg.178]

Reynolds number Friction factor 1C pipe 1C fittir s K-total [Pg.179]


In an axisymmetric flow regime all of the field variables remain constant in the circumferential direction around an axis of symmetry. Therefore the governing flow equations in axisymmetric systems can be analytically integrated with respect to this direction to reduce the model to a two-dimensional form. In order to illustrate this procedure we consider the three-dimensional continuity equation for an incompressible fluid written in a cylindrical (r, 9, 2) coordinate system as... [Pg.113]

Simplified forms of Eq. (6-8) apply to special cases frequently found in prac tice. For a control volume fixed in space with one inlet of area Ai through which an incompressible fluid enters the control volume at an average velocity Vi, and one outlet of area Ao through which fluid leaves at an average velocity V9, as shown in Fig. 6-4, the continuity equation becomes... [Pg.632]

Dynamic analysis of piston flow reactors is fairly straightforward and rather unexciting for incompressible fluids. Piston flow causes the d5mamic response of the system to be especially simple. The form of response is a hmiting case of that found in real systems. We have seen that piston flow is usually a desirable regime from the viewpoint of reaction yields and selectivities. It turns out to be somewhat undesirable from a control viewpoint since there is no natural dampening of disturbances. [Pg.531]

The general approach for kinetic optiaization of open i tubular columns has been to adopt the familiar Golay equation T (equation 1.34) and to assuae that the aobile phase can be approximated by an incompressible fluid with ideal gas properties, (44-50). Circumstances that are approximate at best but serve adequately to demonstrate some of the fundamental characteristics of open tubular columns operated at low fluid densities. The column plate height equation can be written in the form given in M equation (6.1)... [Pg.310]

Eq. (9-17) reduces identically to the Bernoulli equation for an incompressible fluid in a straight, uniform pipe, which can be written in the form... [Pg.271]

Equation (7.27) will hold for incompressible fluids and for compressible fluids with small values of AP. If the pressure gradient across the bed is large and the fluid is compressible, equation (7.27) takes the form... [Pg.52]

The separation process shown in Fignre 2.35a consists of the formation of two new interfaces, each of nnit cross-sectional area, at a location where no interface previously existed. The free energy change associated with the separation process comes directly from the definition of surface energy [Eq. (2.61)] where two snrfaces of unit surface area are formed. With appropriate assumptions regarding constant temperature, pressure, and incompressible fluids, we can equate this free energy change with the... [Pg.200]

In order to familiarize the reader with Prandtl s evaluation procedure [3-5] on which the algebraic method is based, let us examine the steady laminar motion of a fluid along a plate and denote by x the coordinate along the plate, by y the distance to the plate, by u and v the x and y components of the velocity, and by p the pressure. The equations of motion of an incompressible fluid of density p and kinematic viscosity v have the form... [Pg.15]

For the steady flow of an incompressible fluid, state the appropriate mass-continuity equation in spherical coordinates. What can be inferred from the reduced continuity equation about the functional form of of the circumferential velocity v 2... [Pg.195]

Neglect the effects of viscous work (i.e., viscous dissipation), and compare with the steady-state form of the thermal-energy equation for an incompressible fluid. Are they the same equation If so, why If not, why ... [Pg.198]

For an incompressible fluid, the continuity equation is written in general vector form as... [Pg.242]

Consider the flow of an incompressible fluid in the entry region of a circular duct, assuming that the inlet velocity profile is flat. As is often the case, the problem can be generalized by casting into a nondimensional form. A set of nondimensional variables may be chosen as... [Pg.327]

A supercritical fluid is in a state where matter is compressible and behaves as a gas (i.e., it fills and takes the shape of its container), which is not the case when it is in a liquid state (an incompressible fluid that occupies the bottom of its container). Moreover, a supercritical fluid has the typical density of a liquid (between 0.1 and 1.0 g/mL), which results in its characteristic dissolving power. Thus, a supercritical fluid can be defined as a heavy gas with a controllable dissolving power or as a form of matter in which the liquid and gaseous state are indistinguishable [16-18]. [Pg.416]

The equation in either of these last two forms is known as Bernoulli s theorem, in honor of Daniel Bernoulli, who presented it in 1738. Note that Bernoulli s theorem is for a frictionless, incompressible fluid only. [Pg.400]

Determine an expression for the isothermal flow of an incompressible fluid on an inclined plane, assuming that the film thickness is 8 and the angle formed by the plane with the vertical is P (see Fig. P13.12.1). Assume that the flow behavior of the fluid is described by a power law equation. [Pg.578]

Assume there is an incompressible fluid flow with a constant density p the above equation can then be simplified as a very important special form of the continuity equation... [Pg.249]

Here, p is the fluid density and /, is the fluid velocity in the x, direction. When an index, such as i, is repeated in the same term, it means that the term is a summation over all possible values of the index. The first term on the left-hand side describes the change in fluid density over time, and the second term describes the transport of the fluid. For incompressible fluids, which have a constant density, the continuity equation reduces to the following, simpler form ... [Pg.506]

The conventional Reynolds averaging procedure is deduced from the governing equations for incompressible fluid systems. In Cartesian coordinates the corresponding instantaneous equation of continuity takes the following form (i.e., written in a compact form by use Einstein s summation notation) ... [Pg.134]

The original VOF model designed for free surface flow simulations constitutes the mass and momentum conservation equations for incompressible fluids in the jump condition form [155, 108[. [Pg.349]

We begin our analysis with the Navier-Stokes and continuity equations for an incompressible fluid, in their most general dimensional form,... [Pg.309]

Plasma Gas Vapor Liquid An electrically neutral gas made up of ions and electrons. The form of matter that is an easily compressible fluid. The gaseous state of matter. The form of matter that is a relatively incompressible fluid it has a fixed volume, but no fixed shape. [Pg.13]

The momentum equation (1.8) together with the additional constraint of incompressibility (1.3) fully define the motion of an incompressible fluid. They form a system of four scalar equations for four unknown functions the three components of the velocity field and the pressure field. Note that there is no evolution equation for the pressure field, which is given implicitly through the incompressibility condition. This somewhat complicates the analysis and numerical solution of the Navier-Stokes equation. [Pg.4]

Form-friction losses in the Bernoulli equation. Form-friction losses are incorporated in the term of Eq. (4.32). They are combined with the skin-friction losses of the straight pipe to give the total friction loss. Consider, for example, the flow of incompressible fluid through the two enlarged headers, the connecting... [Pg.107]


See other pages where Form incompressible fluid is mentioned: [Pg.178]    [Pg.178]    [Pg.180]    [Pg.304]    [Pg.57]    [Pg.261]    [Pg.77]    [Pg.82]    [Pg.180]    [Pg.304]    [Pg.166]    [Pg.686]    [Pg.809]    [Pg.25]    [Pg.429]    [Pg.841]    [Pg.311]   
See also in sourсe #XX -- [ Pg.178 , Pg.179 , Pg.180 ]




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