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Asymptotic analysis

At a distance sufficiently large for the potential V to have reached its asymptotic behaviour in each arrangement valley, the wavefunction can be [Pg.100]

The quantities inside the ket in (3.28) and (3.29) are evaluated at p=Pmax-Similar expressions hold for the irregular asymptotic matrices and The matching equations are obtained from the condition that the numerically integrated logarithmic derivative matrix Z is equal to its asymptotic form. Imposing K- matrix boundary conditions, we have [Pg.101]

K- and S- matrices can be partitioned into parts which include the coupling (1) only between open channels, (2) only between closed channels, and (3) between open and closed channels. [Pg.101]

A remark on flux conservation. In the traditional inelastic scattering theory, one shows that the logarithmic derivative matrix Z is a symmetric matrix, because of the symmetry of coupling matrices. Moreover, the Wronskian of asymptotic functions is unity and it is easy to show that the K-matrix is symmetric and the S-matrix symmetric and unitary. In reactive collisions, the symmetry of the logarithmic derivative matrix is destroyed by the transformation (3.24) because U. Also, the matrix Wronskian of the asymptotic [Pg.101]

It is fortunate that in the previous problem the normal stress balance is satisfied by the spherical drop profile r = a. However, no satisfactory proof that this is the only solution that has been given. Indeed, one may anticipate some deviation in shape when inertial effects are considered. If one assumes that this deviation is small so that the profile is given by r = a(l + ) with l l 1, then from the symmetry, is a function of 0 alone. If the drop is to have the same volume, thrai [Pg.397]

Similarly, if the drop is to have its center of mass at the origin, then [Pg.397]

Taylor and Acrivos (1964) found an approximate expression for applicable for small valnes of the Reynolds nnmbCT (= l/ap /fi ) and capillary number (= U]4gly). They first obtained the creeping flow solution that satisfied all boundary conditions, those at the drop-flnid intaface being satisfied at r = a. The normal stress balance (Equation 7.19), which was not used in this initial proce-dnre, was then applied, with evaluated at r = a to obtain a first approximation [Pg.398]

in order to determine the deviation from spherical shape, it was necessary to include higher order terms proportional to IP in the stream function. However, such a term emphasizes inertial forces which are not accounted for in the biharmonic equation (Equation 7.21). Proudman and Pearson (1957) have shown how to correct the biharmonic equation for small effects of inertia and obtained the solution for a perfect sphere. The stream function takes the formt Ji + Nr,.  [Pg.398]

Taylor and Acrivos (1964) made the solution satisfy the boundary conditions on the surface r = a, but satisfied the normal stress boundary condition on the surface of a slightly deformed sphere a(l + )) by using a Taylor series expansion to express any functiony(r) at the interface as j a) + Since [Pg.398]


This scheme makes it possible to propagate g from small p where g should vanish to large p where an asymptotic analysis can be performed. [Pg.977]

We have expressed P in tenns of Jacobi coordinates as this is the coordmate system in which the vibrations and translations are separable. The separation does not occur in hyperspherical coordinates except at p = oq, so it is necessary to interrelate coordinate systems to complete the calculations. There are several approaches for doing this. One way is to project the hyperspherical solution onto Jacobi s before perfonning the asymptotic analysis, i.e. [Pg.977]

C. EYopagadon Scheme and Asymptotic Analysis V. Summary and Conclusions... [Pg.179]

Moet H.J.K. (1982) Asymptotic analysis of the boundary in singularly perturbed elliptic variational inequalities. Lect. Notes Math. 942, 1-17. [Pg.382]

Sung, C.J., Makino, A., and Law, C.K., On stretch-affected pulsating instability in rich hydrogen/air flames Asymptotic analysis and computation. Combust. Flame, 128, 422, 2002. [Pg.127]

Including capillary condensation with the Hertz approximation, as considered by Fogden and White [20], introduces pressure outside the contact area i.e., adhesion enters the problem nonenergetically through the tensile normal stress exerted by the condensate in an annulus around the contact circle. The resulting equations cannot be solved analytically however, their asymptotic analysis may be summarized as follows. [Pg.24]

Asymptotic analysis, electronic states, triatomic quantum reaction dynamics, 317—318 Azulene molecule, direct molecular dynamics, complete active space self-consistent field (CASSCF) technique, 408-410... [Pg.68]

An asymptotic analysis for a large activation energy or small reaction zone obtains 2 instead of 3 for the constant [8]. [Pg.92]

As shown in Peters (2000), a rigorous derivation of the flamelet equations can be carried out using a two-scale asymptotic analysis. [Pg.222]

Coleman, T. F., and Conn, A. R., Nonlinear programming via an exact penalty function asymptotic analysis, Math. Prog. 24, 123 (1982). [Pg.253]

ASYMPTOTIC ANALYSIS OF FLAME STRUCTURE PREDICTING CONTAMINANT PRODUCTION... [Pg.406]

Trevino, C., and F. A. Williams. 1988. Asymptotic analysis of the structure and extinction of methane-air diffusion flames. In Dynamics of reactive systems. Part I Flames. Eds. A. L. Kuhl, J. R. Bowen, J.-C. Leyer, and A. A. Borisov. AlAA progress in astronautics and aeronautics ser. Washington, DC American Institute of Aeronautics and Astronautics 113 129-65. [Pg.423]

Card, J. M., and F. A. Williams. 1992. Asymptotic analysis of the structure and extinction of spherically symmetrical n-heptane diffusion flames. Combustion Science Technology 84 91-119. [Pg.423]

Hewson, J. C., and F.A. Williams. 1998. Rate-ratio asymptotic analysis of methane-air diffusion-flame structure for predicting production of oxides of nitrogen. Combustion Flame 117 441-76. [Pg.424]

Bai, X. S., and K. Seshadri. 1997. Rate-ratio asymptotic analysis of nonpremixed methane flames. Combustion Theory Modeling 3 51-75. [Pg.424]

Yang, B., and K. Seshadri. 1992. Asymptotic analysis of the structure of nonpremixed methane-air flames using reduced chemistry. Combustion Science Technology 88 115-32. [Pg.424]

In multiscale asymptotic analysis of reaction network we found several very attractive zero-one laws. First of all, components eigenvectors are close to 0 or +1. This law together with two other zero-one laws are discussed in Section 6 "Three zero-one laws and nonequilibrium phase transitions in multiscale systems". [Pg.111]

The asymptotic analysis of multiscale systems for log-uniform distribution of independent constants on an interval log k e[a, fk] (—a, ji- co) is possible, but parameters a, /) do not present in any answer, they just should be sufficiently big. A natural question arises, what is the limit It is a log-uniform distribution on a line, or, for n independent identically distributed constants, a log-uniform distribution on R"). [Pg.123]

The idea of dominant subsystems in asymptotic analysis was proposed by Newton and developed by Kruskal (1963). A modern introduction with some historical review is presented by White. In our analysis we do not use the powers of small parameters (as it was done by Akian et al., 2004 Kruskal, 1963 Lidskii, 1965 Vishik and Ljustemik, 1960 White, 2006), but operate directly with the rate constants ordering. [Pg.164]

White, R. B., "Asymptotic Analysis of Differential Equations". Imperial College Press World Scientific, London (2006). [Pg.168]


See other pages where Asymptotic analysis is mentioned: [Pg.977]    [Pg.213]    [Pg.214]    [Pg.215]    [Pg.770]    [Pg.934]    [Pg.110]    [Pg.123]    [Pg.331]    [Pg.153]    [Pg.62]    [Pg.75]    [Pg.93]    [Pg.95]    [Pg.101]    [Pg.102]    [Pg.283]    [Pg.317]    [Pg.318]    [Pg.319]    [Pg.103]    [Pg.60]    [Pg.65]    [Pg.123]   
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