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Perturbative equations transfer rate

In order for a process to be controllable by machine, it must represented by a mathematical model. Ideally, each element of a dynamic process, for example, a reflux drum or an individual tray of a fractionator, is represented by differential equations based on material and energy balances, transfer rates, stage efficiencies, phase equilibrium relations, etc., as well as the parameters of sensing devices, control valves, and control instruments. The process as a whole then is equivalent to a system of ordinary and partial differential equations involving certain independent and dependent variables. When the values of the independent variables are specified or measured, corresponding values of the others are found by computation, and the information is transmitted to the control instruments. For example, if the temperature, composition, and flow rate of the feed to a fractionator are perturbed, the computer will determine the other flows and the heat balance required to maintain constant overhead purity. Economic factors also can be incorporated in process models then the computer can be made to optimize the operation continually. [Pg.39]

Rates of non-adiabatic intramolecular electron transfer were calculated in Ref. [331] using a self-consistent perturbation method for the calculation of electron-transfer matrix elements based on Lippman-Schwinger equation for the effective scattering matrix. Iteration of this perturbation equation provides the data that show the competition between the through-bond and through-space coupling in bridge structures. [Pg.83]

This equation can be used for solving many problems. Its only restriction is that the perturbation is weak. Because of the general applicability of this equation it is named Fermi s golden rule of quantum mechanics. This rule has been applied in many quantum mechanical derivations of the electron transfer rate without its being particularly mentioned. One can identify it immediately by the appearance of the I V term in a relevant equation. We return to this point in the following sections. [Pg.149]

Bardeen considers two separate subsystems first. The electronic states of the separated subsystems are obtained by solving the stationary Schrodinger equations. For many practical systems, those solutions are known. The rate of transferring an electron from one electrode to another is calculated using time-dependent perturbation theory. As a result, Bardeen showed that the amplitude of electron transfer, or the tunneling matrix element M, is determined by the overlap of the surface wavefunctions of the two subsystems at a separation surface (the choice of the separation surface does not affect the results appreciably). In other words, Bardeen showed that the tunneling matrix element M is determined by a surface integral on a separation surface between the two electrodes, z = zo. [Pg.22]

The possible effect of a coupled chemical reaction on the response to an electrochemical perturbation can be deduced by combination of the j F vs. surface concentration relation with the proper rate equation for the charge transfer process and subsequent elaboration applying to a particular method. Naturally, a complex rate equation will be unfavourable if it is... [Pg.331]

In real situations, the question arises frequently as to whether or not a marked influence of heat and mass transfer on the observable reaction rate may be expected under certain reaction conditions. Quite often then, one has to deal with reactions obeying complex kinetics where either none or only a very cumbersome analytical solution is possible based upon the methods described in Section 6.2.3. For such cases a number of useful diagnostic criteria have been developed in the past, either derived from asymptotic solutions of the governing differential equations or from perturbation methods [86], Most of these criteria have been explained in a detailed review by Mears [76]. More recent surveys of diagnostic transport criteria have been given by Butt [12] and by Madon and Boudart [74],... [Pg.347]

When P(E) is not perturbed by the reaction, so that the distribution of critically energized molecules is that characteristic of equilibrium, the RRK model leads to a specific first-order rate constant of the form k = A exp —E /RT) where A is the frequency of internal energy transfer between oscillators. The Slater formulation in these circumstances gives k = V exp —E /RT ), both results being similar in form to the Arrhenius equation. The A factor in the RRK model represents the frequency of energy transfer between oscillators, which Jor weakly coupled oscillators would be of the order of their beat frequencies, or about 10 to 10 sec In the Slater model, V represents a weighted rms frequency of the normal frequencies which describe the decomposition [Eq. (X.6.1)]... [Pg.220]

Equations 5E and 6E are special cases of a general rule according to which, whenever a system is perturbed to a small extent, the response is proportional to the magnitude of the perturbation. But how small is "small" in the present context This must be defined in some unitless form, comparing affinity to thermal energy or rate to exchange rate. For Eq. 5E the perturbation is small if A/RT 1. Likewise for the case of charge transfer we should have riF/RT 1. Clearly, a small perturbation also leads to v/v 1 and i/i 1. This latter... [Pg.374]

The space velocity, often used in the technical literature, is the total volumetric feed rate under normal conditions, F o(Nm /hr) per unit catalyst volume (m X that is, PbF o/W. It is related to the inverse of the space time W/F g used in this text (with W in kg cat. and F q in kmol A/hr). It is seen that, for the nominal space velocity of 13,800 (m /m cat. hr) and inlet temperatures between 224 and 274 C, two top temperatures correspond to one inlet temperature. Below 224 C no autothermal operation is possible. This is the blowout temperature. By the same reasoning used in relation with Fig. 11.5.e-2 it can be seen that points on the left branch of the curve correspond to the unstable, those on the right branch to the upper stable steady state. The optimum top temperature (425°C), leading to a maximum conversion for the given amount of catalyst, is marked with a cross. The difference between the optimum operating top temperature and the blowout temperature is only 5°C, so that severe control of perturbations is required. Baddour et al. also studied the dynamic behavior, starting from the transient continuity and energy equations [26]. The dynamic behavior was shown to be linear for perturbations in the inlet temperature smaller than 5°C, around the conditions of maximum production. Use of approximate transfer functions was very successful in the description of the dynamic behavior. [Pg.512]

Bearing in mind that the nuclear spin system is an ensranble perturbed by the rf-field, we have to consider the possibility that energy from the rf-field is transferred to the nuclear spins and dissipated further to the crystal lattice. These effects can be described by relaxation times that characterize the rates with which the system returns to thermal equilibrium after the perturbation has been switched off. There are the longitudinal or spin-lattice relaxation time Tj and the transverse or spin-spin relaxation time Tj. Including the relaxation effects the equations of motion in the rotating frame (cf. Eq. (19)) are... [Pg.102]

It has also been observed that the rate constants for electron transfer in simple eomplexes can be perturbed by ion-pair formation in ways that depend on the energy of the IPCT transition and on the electronic structure of the reactants. The observed effects can most simply be discussed with reference to Equations (52)-(54). [Pg.682]


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See also in sourсe #XX -- [ Pg.123 , Pg.124 , Pg.125 , Pg.126 , Pg.127 ]




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Equation transfer

Transfer rate

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