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Forward difference method

Analogous to the forward-difference method previously discussed, it is only first-order accurate in At. The only formal difference with respect to the forward-difference equation (8-10) appears to be the fact that the space derivative is evaluated at time tn+i, not at time tn. [Pg.227]

The implicit backward-difference algorithm does not show the stability problems encountered in the case of the explicit forward-difference method, and this results immediately by analyzing the expression of the amplification factor ... [Pg.228]

The terminology originally suggested (17) for the methods based on Eqs. (174) or (175) is, respectively, the adjoint-difference method or the adjoint-difference approximation. The method based on Eq. (177) has been termed (45) the forward-difference method. The terminology we use is consistent with the terminology used for other perturbation-based methods dealt with in this review. [Pg.225]

Figures 12.11 shows plots of yj = y x = 0.2) as a function of time. Computations from the forward difference scheme are shown in Fig. 12.11a, while those of the backward difference and the Crank-Nicolson schemes are shown in Figs. 12.11h and c, respectively. Time step sizes of 0.01 and 0.05 are used as parameters in these three figures. The exact solution (Eq. 12.129) is also shown in these figures as dashed lines. It is seen that the backward difference and the Crank-Nicolson methods are stable no matter what step size is used, whereas the forward difference scheme becomes unstable when the stability criterion of Eq. 12.139 is violated. With the grid size of Aa = 0.2, the maximum time step size for stability of the forward difference method is At = (Ajc)V2 = 0.02. Figures 12.11 shows plots of yj = y x = 0.2) as a function of time. Computations from the forward difference scheme are shown in Fig. 12.11a, while those of the backward difference and the Crank-Nicolson schemes are shown in Figs. 12.11h and c, respectively. Time step sizes of 0.01 and 0.05 are used as parameters in these three figures. The exact solution (Eq. 12.129) is also shown in these figures as dashed lines. It is seen that the backward difference and the Crank-Nicolson methods are stable no matter what step size is used, whereas the forward difference scheme becomes unstable when the stability criterion of Eq. 12.139 is violated. With the grid size of Aa = 0.2, the maximum time step size for stability of the forward difference method is At = (Ajc)V2 = 0.02.
The method described by Equation 9.94 to Equation 9.98 is an explicit method and is commonly called the forward difference method. It is explicit because knowledge of Wjj for j at all the grid points means that... [Pg.417]

The forward difference method is considered conditionally stable. Further, it can be shown that the method converges with a rate of convergence on the order of k + /t ) if the condition... [Pg.418]

Contrasting the forward difference method is the implicit method of Crank-Nicolson [5,9,18,22,25]. The difference formulation for the homogeneous case of Equation 9.90 with zero end conditions is... [Pg.418]

The Crank-Nicolson method is unconditionally stable. However, it does require the solution of simultaneous equations. Also, this method is more accurate than the forward difference method. [Pg.418]

Figure 6i19l Mesh points for the forward difference method. Figure 6i19l Mesh points for the forward difference method.
In order to solve the PDE, the initial and boundary conditions also need to be specified. The explicit forward difference method is of little practical use because the method is only conditionally stable. This can be understood better by looking at file relationship between the unknown value and the values known from previous time steps, as in the stencil in Figure 6.20. [Pg.111]

As the local error is the same as in the forward difference method, i.e. 0 k) + OQp-), the error from the time discretization dominates, assuming step sizes and h k. Although the method is unconditionally stable, its accuracy is low due to the large local truncation error. Overall, the backward difference method is 0 k), which means that the error at a certain point decreases linearly with k. In other words, if k is cut in half, so is the error. In contrast, if h is cut in half (for a given K), the error would be about the same, and the amount of computation would increase. [Pg.113]

A rather different method from the preceding is that based on the rate of dissolving of a soluble material. At any given temperature, one expects the initial dissolving rate to be proportional to the surface area, and an experimental verification of this expectation has been made in the case of rock salt (see Refs. 26,27). Here, both forward and reverse rates are important, and the rate expressions are... [Pg.577]

The described method can generate a first-order backward or a first-order forward difference scheme depending whether 0 = 0 or 0 = 1 is used. For 9 = 0.5, the method yields a second order accurate central difference scheme, however, other considerations such as the stability of numerical calculations should be taken into account. Stability analysis for this class of time stepping methods can only be carried out for simple cases where the coefficient matrix in Equation (2.106) is symmetric and positive-definite (i.e. self-adjoint problems Zienkiewicz and Taylor, 1994). Obviously, this will not be the case in most types of engineering flow problems. In practice, therefore, selection of appropriate values of 6 and time increment At is usually based on trial and error. Factors such as the nature of non-linearity of physical parameters and the type of elements used in the spatial discretization usually influence the selection of the values of 0 and At in a problem. [Pg.66]

Euler s method for solving the above set of ODEs uses a first-order, forward difference approximation in the -direction. Equation (8.16). Substituting this into Equation (8.21) and solving for the forward point gives... [Pg.275]

The third kind boundary conditions. The first kind boundary conditions we have considered so far are satisfied on a grid exactly. In Chapter 2 we have suggested one effective method, by means of which it is possible to approximate the third kind boundary condition for the forward difference scheme (a = 1) and the explicit scheme (cr = 0) and generate an approximation of 0 t -b h ). Here we will handle scheme (II) with weights, where cr is kept fixed. In preparation for this, the third kind boundary condition... [Pg.321]

This estimate can be improved for the forward difference scheme with (7 = 1 by means of the maximum principle and the method of extraction of stationary nonhomogeneities , what amounts to setting... [Pg.474]

Having no opportunity to touch upon this topic, we refer the readers to the aforementioned chapters of the manograph The Theory oof Difference Schemes , in which the method of extraction of stationary nonhomogeneities was employed with further reference to a priori estimates of z. The forward difference scheme with cr = 1 converges uniformly with the rate 0 h + r) due to the maximum principle. [Pg.495]

The use of multiple otherwise incompatible catalysts allows multistep reactions to proceed in one reaction vessel, providing many potential benefits. In this chapter, literature examples of nanoencapsulation for the purpose of process intensification have been discussed comprehensively. Current efforts in the literature are mostly concentrated in the areas of LbL template-based nanoencapsulation and sol-gel immobilization. Other cascade reactions (without the use of nanoencapsulation) that allow the use of incompatible catalysts were also examined and showcased as potential targets for nanoencapsulation approaches. Finally, different methods for nanoencapsulation were investigated, thereby suggesting potential ways forward for cascade reactions that use incompatible catalysts, solvent systems, or simply incompatible reaction conditions. [Pg.159]

Beyond the formal comparison of different methods, Kremer16 has put forward an original system whereby governments would acquire the patent from its creators at its social value and transfer it to the public domain. The author acknowledges the difficulty of establishing the social value of an innovation, but proposes an invitation to tender to determine the private value of a patent. [Pg.30]

Finite difference Newton method. Application of Equation (5.8) to/(jc) = x2 - x is illustrated here. However, we use a forward difference formula for f x) and a three-point central difference formula for/"(jc)... [Pg.162]

Different methods can be used to detect cell death in CLL cells. Methods based on detection of cell death by flow cytometry are recommended as CLL cells are easily distinguishable by forward and size scatter from possible contamination of... [Pg.224]

Table 8.3 Mean and maximum absolute errors (kcal mol ) in enthalpies of activation and forward reaction for different methods... Table 8.3 Mean and maximum absolute errors (kcal mol ) in enthalpies of activation and forward reaction for different methods...
The explicit (or forward) Euler method begins by approximating the time derivative with a first-order finite difference as... [Pg.622]

Equation (5.38) can be interpreted as the scalar product of a forward-moving density and a backward-moving time-dependent operator. The optimal field at time t is determined by a time-dependent objective function propagated from the target time T backward to time t. A first-order perturbation approach to obtain a similar equation for optimal chemical control in Liouville space has been derived in a different method by Yan et al. [28]. [Pg.245]

Fig. 4.3. Different methods of plotting one set of two-dimensional (forward scatter vs. side scatter) data. A Two separate histograms, a dot plot, a three-dimensional plot, and contour plots according to two different plotting algorithms. B Four additional contour plotting algorithms for the same data. Fig. 4.3. Different methods of plotting one set of two-dimensional (forward scatter vs. side scatter) data. A Two separate histograms, a dot plot, a three-dimensional plot, and contour plots according to two different plotting algorithms. B Four additional contour plotting algorithms for the same data.
The species balance relation Eq. 13.2-8 is transformed to a difference equation using the forward difference on the time derivative and the backward difference on the space derivative. The finite difference form of the x-momentum equation (Eq. 13.2-25) is obtained by using the forward difference on all derivatives, and is solved by the Crank-Nicolson method. The same is true for the energy equation (Eq. 13.2-26). [Pg.807]

The method of lines is called an explicit method because the new value T(r, z + Az) is given as an explicit function of the old values T(r, z),T(r — Ar, z),. See, for example, Equation (8.57). This explicit scheme is obtained by using a first-order, forward difference approximation for the axial derivative. See, for example, Equation (8.16). Other approximations for dTjdz are given in Appendix 8.2. These usually give rise to implicit methods where T(r,z Az) is not found directly but is given as one member of a set of simultaneous algebraic equations. The simplest implicit scheme is known as backward differencing and is based on a first-order, backward difference approximation for dT/dz. Instead of Equation (8.57), we obtain... [Pg.314]

OPTIMIZATION METHOD DFP WITH FORWARD-DIFFERENCE Number of Structures 3... [Pg.34]


See other pages where Forward difference method is mentioned: [Pg.227]    [Pg.110]    [Pg.227]    [Pg.110]    [Pg.64]    [Pg.264]    [Pg.314]    [Pg.302]    [Pg.256]    [Pg.21]    [Pg.179]    [Pg.302]    [Pg.132]    [Pg.172]    [Pg.294]    [Pg.176]    [Pg.445]    [Pg.36]   
See also in sourсe #XX -- [ Pg.417 ]




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