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Differential coefficient conversion

For a CSTR the stationary-state relationship is given by the solution of an algebraic equation for the reaction-diffusion system we still have a (non-linear) differential equation, albeit ordinary rather than partial as in eqn (9.14). The stationary-state profile can be determined by standard numerical methods once the two parameters D and / have been specified. Figure 9.3 shows two typical profiles for two different values of )(0.1157 and 0.0633) with / = 0.04. In the upper profile, the stationary-state reactant concentration is close to unity across the whole reaction zone, reflecting only low extents of reaction. The profile has a minimum exactly at the centre of the reaction zone p = 0 and is symmetric about this central line. This symmetry with the central minimum is a feature of all the profiles computed for the class A geometries with these symmetric boundary conditions. With the lower diffusion coefficient, D = 0.0633, much greater extents of conversion—in excess of 50 per cent—are possible in the stationary state. [Pg.244]

To demonstrate the superior dynamic controllability of high-conversion and low-temperature designs, the nonlinear differential equations are numerically integrated for the four different design cases. Disturbances in feed flowrate, temperature controller set-point, and overall heat-transfer coefficient are made, and the peak deviations in reactor... [Pg.117]

Experimentally, the CD intensity is often quantified by the differential molar absorption coefficient Ae = l — r for the absorption of left-handed vs right-handed circular polarized light, where Ae and e are usually in units of L mol 1 cm-1. The conversion from Ae in L moP1 cm-1 to the molar ellipticity in deg cm2 dmoP1 is [0] = (18,0001n(10)/47r)Ae. The connection with quantities that can be calculated from first-principles theory is given by the following equation [35] ... [Pg.7]

Step 3. The exothermic heat of reaction must be removed, and the reactor feed must be heated to a high enough temperature to initiate the reaction. Since the heat of reaction is not large and complete one-pass conversion is not achieved, the reactor exit temperature is only 32°F higher than the reactor inlet temperature. Since heat transfer coefficients in gas-to-gas systems are typically quite low, this small temperature differential would require a very large heat exchanger if only the reactor effluent is used to heat the reactor feed and no furnace... [Pg.276]

The recommended unit for MCD spectroscopy, Aem, is based on the extinction coefficient for differential absorbance of a 1M solution of the solute at a field strength of 1 T. The original 9 ellipicity unit is still sometimes used. The conversion factors are 6 = 32.98 AA, where 9 is expressed in units of mdeg or [0]m = 3298A6m where, [0]m is expressed in units of deg cm -dmol . Room temperature spectral measurements are usually measured in solution, ideally in a solvent which is optically transparent in the 280-1000 nm region. [Pg.6070]

Values of the coefficients for the set of differential equations were chosen to give cool flames at realistic initial pressures and temperatures. Further restrictions on the choice of coefficients were imposed by requiring that the fuel conversion should not exceed 25 % at the maximum of the temperature pulse, that the induction period should be between 15 and 20 sec, and that the thermal relaxation time should be 0,25 sec. To achieve this the rate coefficients of reactions (d), (f), (h) and (g) were varied about reasonable estimates of their likely values. The parameters chosen for the model are given in Table 24. The computer was used in a conversational mode to map out an ignition diagram (Fig. 26) which compares favourably with that found experimentally [191] (Fig. 27). [Pg.347]

A mathematical model for styrene polymerization, based on free-radical kinetics, accounts for changes in termination coefficient with increasing conversion by an empirical function of viscosity at the polymerization temperature. Solution of the differential equations results in an expression that calculates the weight fraction of polymer of selected chain lengths. Conversions, and number, weight, and Z molecular-weight averages are also predicted as a function of time. The model was tested on peroxide-initiated suspension polymerizations and also on batch and continuous thermally initiated bulk polymerizations. [Pg.13]

By flash excitation of this reaction system, it is not only possible to measure the absorbance change at 870 nm produced by photooxidation of the primary electron donor but also that at 550 nm produced by the oxidation of cytochrome c, as shown in Fig. 12, lower right trace. Since the differential extinction coefficient of cytochrome c was precisely known, the authors were able to use the differential extinction coefficient of P870 commonly accepted at the time, and the measured amplitudes of absorbance changes at 870 and 550 nm, to calculate a stoichiometry of 1 P870 1 cyt c for this reaction. Parson and Clayton " later utilized this model system to obtain conversely a more accurate differential extinction coefficient of 128 mM -cm" forP870 (see Section II. of Chapterd for further details). [Pg.195]

Combining these two equations yields a differential equation which has to be solved including adequate boundary conditions. The overall conversion of NO as a function of the film mass-transfer coefficient, the effective diffusivity, the linear velocity, and the first-order rate constant, is obtained with structural parameters of the honeycomb. [Pg.161]

By the use of the above differential method for the determination of k,. and kp, we have in fact determined kG and kp as a function of time (see Eqs. (27) and (31)) thus, these rate coefficients are not the usual rate constants which are commonly obtained by the conventional integral method. (The reader is reminded, that in the fundamental scenarios, kc and kp were treated as real constants to enable the integration of differential equations.) Our experiments (see later) have proven that kc and kp are not true rate constants but are functions of time or conversion (see e.g., Figs. 13A and 13C and sect. 4.1.1.1). [Pg.48]

When the rate coefficient, ft(hr ), is known, Eq. 1.3-4 permits the calculation of the rate, r, for any concentration of the reacting component. Conversely, when the change in concentration is known as a funaion of time, Eq. (1.3-4) permits the calculation of the rate coefficient. This method for obtaining k is known as the differential method further discussion will be presented later. [Pg.8]

For noncatalytic homogeneous reactions, a tubular reactor is widely used because it cai handle liquid or vapor feeds, with or without phase change in the reactor. The PFR model i usually adequate for the tubular reactor if the flow is turbulent and if it can be assumed tha when a phase change occurs in the reactor, the reaction takes place predominantly in one o the two phases. The simplest thermal modes are isothermal and adiabatic. The nonadiabatic nonisothermal mode is generally handled by a specified temperature profile or by heat transfer to or from some specified heat source or sink and a corresponding heat-transfer area and overall heat transfer coefficient. Either a fractional conversion of a limiting reactant or a reactoi volume is specified. The calculations require the solution of ordinary differential equations. [Pg.214]

Ideal case. Note that the majority of materials do not present a constant Seebeck coefficient, which can, in principle, be translated by the indication on the previous graph of a second fector, called differential factor of coupling, for connecting the energies-per-entity (efforts and flows) as appropriate for a conversion with variable coupling. The coupling fector in this case can be seen, physically speaking, as a manifestation of an additional effect, called Thomson effect, treated in case study Jll. [Pg.653]

Nernst s equations were soon adopted by other workers although they often multiplied the ratio of concentrations by the ratio of molar conductances to allow for incomplete dissociation (even for strong electrolytes). Only in 1920 did Macinnes and Beattie (1 ) replace concentrations by activities and use the emf equation in its proper differential form. A more general equation in terms of ion-constituent transference numbers and applicable also to electrodes reversible to a complex ion was later derived by the present author (H). In 1935 Brown and Macinnes (92) initiated the converse procedure of calculating activity coefficients from the accurate m.b. transference numbers then available and the emfs of cells with transference, an approach that required only one type of reversible electrode. [Pg.108]

Let us now look at the interrelations holding between the material coefficients listed in Table 4.2. In the context of coupling effects it has already been shown that the direct and the converse piezoelectric effects are described by identical material coefficients. This follows immediately from their definition as second derivatives of the associated thermodynamic potential, recognizing the fact that the order of differentiations may be reversed. Direct and converse effects are described by relations between different pairs of variables. The equality of the coefficients governing the direct and the converse effects reduces the number of independent material coefficients for each selection of the triple of independent variables. It does not, however, represent a relation between material coefficients derived from different thermodynamic potentials. [Pg.64]


See other pages where Differential coefficient conversion is mentioned: [Pg.213]    [Pg.30]    [Pg.103]    [Pg.474]    [Pg.1534]    [Pg.326]    [Pg.483]    [Pg.51]    [Pg.414]    [Pg.205]    [Pg.366]    [Pg.374]    [Pg.302]    [Pg.231]    [Pg.288]    [Pg.517]    [Pg.531]    [Pg.392]    [Pg.9]    [Pg.426]    [Pg.76]    [Pg.194]    [Pg.35]    [Pg.210]    [Pg.93]    [Pg.53]    [Pg.720]    [Pg.525]    [Pg.355]    [Pg.2110]   
See also in sourсe #XX -- [ Pg.267 ]




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