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The Steady State Equations

The actual number of steady states of our three CSTR system can be found by solving the steady-state equations of Section 6.4.3. [Pg.419]

For more details on multiplicity and bifurcation, see the Appendix with this title. [Pg.419]

The steady-state equations for (6.144) are given by the nine transcendental equations of the system of equations F(X) = 0. For the steady state, we can reduce each set of three equations for one tank to a single transcendental equation as explained below. [Pg.419]

For example, for tank 1 the steady-state version of the DE (6.135) becomes [Pg.419]

This equation obtained as usual by setting the derivative in (6.135) equal to zero. Equation (6.145) makes [Pg.419]


On subsciCuLlng (12.49) into uhe dynamical equations we may expand each term in powers of the perturbations and retain only terms of the zeroth and first orders. The terms of order zero can then be eliminated by subtracting the steady state equations, and what remains is a set of linear partial differential equations in the perturbations. Thus equations (12.46) and (12.47) yield the following pair of linearized perturbation equations... [Pg.172]

In a vessel with axial dispersion, the steady-state equation for a reaction of order q is... [Pg.2089]

Applying the steady state equations for the free radieals H, CH3, and C2H5, the rate of formation of ethylene C2H4 for a eonstant volume bateh reaetor is ... [Pg.44]

In Fig. 7A is given the steady state scheme for two sites which defines each of the elemental rate constants and in Fig. 7B are the steady state equations for the rate of change with time of the probability, %, of each of the occupancy states of the channel oo, xo, ox and xx. C and Cx are the concentrations of the x ion on the left-and right-hand sides, respectively. The general expression for the current, ix, due to the ionic species, x, passing through a single channel is... [Pg.190]

A mechanical system, typified by a pendulum, can oscillate around a position of final equilibrium. Chemical systems cannot do so, because of the fundamental law of thermodynamics that at all times AG > 0 when the system is not at equilibrium. There is nonetheless the occasional chemical system in which intermediates oscillate in concentration during the course of the reaction. Products, too, are formed at oscillating rates. This striking phenomenon of oscillatory behavior can be shown to occur when there are dual sets of solutions to the steady-state equations. The full mathematical treatment of this phenomenon and of instability will not be given, but a simplified version will be presented. With two sets of steady-state concentrations for the intermediates, no sooner is one set established than the consequent other changes cause the system to pass quickly to the other set, and vice versa. In effect, this establishes a chemical feedback loop. [Pg.190]

The steady-state equations allow evaluation of the possible steady operating points. [Pg.341]

As soon as we finish the first-order Taylor series expansion, the equation is linearized. All steps that follow are to clean up the algebra with the understanding that terms of the steady state equation should cancel out, and to change the equation to deviation variables with zero initial condition. [Pg.36]

Dividing by 4nAr and letting Ar go to zero yields the steady-state equation... [Pg.707]

Under all but laminar flow conditions, the steady-state pipeline network problems are described by mixed sets of linear and nonlinear equations regardless of the choice of formulations. Since these equations cannot be solved directly, an iterative procedure is usually employed. For ease of reference let us represent the steady-state equations as... [Pg.148]

The limitation of the prescribed diffusion approach was removed, for an isolated ion-pair, by Abell et al. (1972). They noted the equivalence of the Laplace transform of the diffusion equation in the absence of scavenger (Eq. 7.30) and the steady-state equation in the presence of a scavenger with the initial e-ion distribution appearing as the source term (Eq. 7.29 with dP/dt = 0). Here, the Laplace transform of a function/(t) is defined by... [Pg.234]

These manipulations are not as complicated as they may at first appear, for I have written out the expressions in full detail in order to avoid possible uncertainty about just what the manipulations are. Note that the right-hand sides of these equations are the steady-state equations solved in Section... [Pg.26]

The polymerization kinetics have been intensively discussed for the living radical polymerization of St with the nitroxides,but some confusion on the interpretation and understanding of the reaction mechanism and the rate analysis were present [223,225-229]. Recently, Fukuda et al. [230-232] provided a clear answer to the questions of kinetic analysis during the polymerization of St with the poly(St)-TEMPO adduct (Mn=2.5X 103,MW/Mn=1.13) at 125 °C. They determined the TEMPO concentration during the polymerization and estimated the equilibrium constant of the dissociation of the dormant chain end to the radicals. The adduct P-N is in equilibrium to the propagating radical P and the nitroxyl radical N (Eqs. 60 and 61), and their concentrations are represented by Eqs. (62) and (63) in the derivative form. With the steady-state equations with regard to P and N , Eqs. (64) and (65) are introduced, respectively ... [Pg.116]

This shows that this modified heat of gasification includes all effects that augment or reduce the mass loss rate. Recall that the term in the [ ] becomes zero if the solid is thermally thick and the virgin solid equilibrates to the steady state. Equating Equations (9.107) and (9.108) gives an equation for the flame temperature ... [Pg.276]

The steady state equation for a second order reaction as obtained problem P5.08.01 is,... [Pg.648]

Fig. 3. Arrhenius plots for the decomposition of dimethyl mercury. All rate coefficients are at or near the high-pressure limit. If a radical scavenger has been used it is shown in brackets following the authors names. 1, Krech and Price (benzene) 2, Kallend and Purnell (propene) 3, Russell and Bernstein (cyclopentane) 4, Russell and Bernstein 5, Laurie and Long 6, Kominar and Price (toluene) O, Weston and Seltzer (cyclopentane) , point calculated from the steady-state equation of Kallend and Purnell. Fig. 3. Arrhenius plots for the decomposition of dimethyl mercury. All rate coefficients are at or near the high-pressure limit. If a radical scavenger has been used it is shown in brackets following the authors names. 1, Krech and Price (benzene) 2, Kallend and Purnell (propene) 3, Russell and Bernstein (cyclopentane) 4, Russell and Bernstein 5, Laurie and Long 6, Kominar and Price (toluene) O, Weston and Seltzer (cyclopentane) , point calculated from the steady-state equation of Kallend and Purnell.
Considering that there is geologic evidence that the Ca concentration of the oceans change with time, it is necessary that Fvi,/Fsechanges with time. As noted by De La Rocha and DePaolo (2000), if the steady state equation for the sedimentary values is written as ... [Pg.281]

THE MICHAELIS-MENTEN EQUATION AS A LIMITING CASE OF THE STEADY STATE EQUATION. To achieve a rapid equilibrium between E and EX, ki[S] and k2 must each be much greater than ks. [Note the rate constant ki is a bimolecular rate constant with units of molarity seconds, and we must use ki[S]... [Pg.249]

As the particle traverses from one barrier to the next it changes its energy. The conditional probability kernel P(E E ) that the particle changes its energy from E to E is determined by the energy loss parameter 8 = pA and a quantum parameter a = The quantum kernel is as in Eq. 38. The main difference between the double and single well cases and the periodic potential arises in the steady state equation for the fluxes ... [Pg.23]

For a mechanism with S-1 intermediates in addition to free sites the steady state equations is a system of S equations, at most (S-1) are linearily independent. [Pg.32]

Next one needs an expression for (xA — xA"). The difference in concentration between the two streams results from two effects thermal diffusion, which tends to increase the concentration difference, and convection, which tends to decrease it. Each of these effects is considered separately by obtaining an approximate integrated form of the steady state equation of continuity as applied to that particular process. If the only effect tending to produce a concentration difference were thermal diffusion, then according to Eq. (131) dxA/dx = — (kT/T)(d,T/dx) this expression may be written in difference form over the distance from x = — ( 4)a to x — + (M)° thus ... [Pg.226]

Using eq. (48) and setting up the steady-state equations for [P2 ] in delayed fluorescence and [P ] in normal fluorescence it can be shown that at the low rates of light absorption to which eq. (48) applies, the ratio of delayed to normal fluorescence of the monomer is given by... [Pg.355]

Fig. 15.8 Example problem illustrating the iteration path for the hybrid Newton and time-integration approach (solid lines) and the time-marching approach alone (dashed line). The contours are for the maximum norm of residuals of the steady-state equations. Fig. 15.8 Example problem illustrating the iteration path for the hybrid Newton and time-integration approach (solid lines) and the time-marching approach alone (dashed line). The contours are for the maximum norm of residuals of the steady-state equations.
No theoretical criterion for flammability limits is obtained from the steady-state equation of the combustion wave. On the basis of a model of the thermally propagating combustion wave it is shown that the limit is due to instability of the wave toward perturbation of the temperature profile. Such perturbation causes a transient increase of the volume of the medium reacting per unit wave area and decrease of the temperature levels throughout the wave. If the gain in over-all reaction rate due to this increase in volume exceeds the decrease in over-all reaction rate due to temperature decrease, the wave is stable otherwise, it degenerates to a temperature wave. Above some critical dilution of the mixture, the latter condition is always fulfilled. It is concluded that the existence of excess enthalpy in the wave is a prerequisite of all aspects of combustion wave propagation. [Pg.16]

It is found experimentally that limit mixtures, incapable of supporting combustion waves, nevertheless have theoretical thermodynamic flame temperatures of the order of 1000° C. or more. It is, therefore, not immediately clear why combustion waves, albeit slowly propagating, should not develop in mixtures possessing such substantial chemical enthalpy. The question arises whether the observed limits of flammability are true limits or whether such mixtures are actually capable of supporting combustion waves but are prevented from doing so by experimental limitations. Experimentalists believe that the limits are true. On the other hand, no theoretical criterion for the limit is obtained from the steady-state equations of the combustion wave. That is, the equations describe combustion waves without differentiating between mixtures that are known to be flammable and mixtures that are known to be nonflammable. Therefore, for nonflammable mixtures the combustion wave becomes unstable to perturbations and thus disappears (7). Conversely, for flammable mixtures the combustion wave can overcome perturbations—i.e., it returns to the steady state after being perturbed. [Pg.18]

That is, we are interested in y(r) = Y(r, oo) and the corresponding reaction rate, Kq — K(oo). The former satisfies the equation (3.2.39) with the boundary conditions (3.2.40). As it is clear from Chapter 3, the solution of equation (3.2.39) defines uniquely the survival probability u>(l oo) of geminate pairs. In a particular case of the Coulomb interaction, the solution of the steady-state equation (3.2.39) is simplified since for the unscreened Coulomb potential the relation V2C/(r) = 0 holds. Integrating the differential equation... [Pg.187]


See other pages where The Steady State Equations is mentioned: [Pg.186]    [Pg.53]    [Pg.149]    [Pg.35]    [Pg.36]    [Pg.37]    [Pg.83]    [Pg.88]    [Pg.641]    [Pg.749]    [Pg.129]    [Pg.175]    [Pg.177]    [Pg.233]    [Pg.176]    [Pg.126]    [Pg.167]    [Pg.265]    [Pg.66]    [Pg.20]    [Pg.276]    [Pg.245]    [Pg.14]   


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The State Equations

The Steady State

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