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asymptotic solutions of difference equations

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21: 9.13 Generalized Airy Functions
are used in approximating solutions to differential equations with multiple turning points; see §2.8(v). … As z In Olver (1977a, 1978) a different normalization is used. … Properties and graphs of U m ( t ) , V m ( t ) , V ¯ m ( t ) are included in Olver (1977a) together with properties and graphs of real solutions of the equationand the difference equation
22: Bibliography G
  • W. Gautschi (1997b) The Computation of Special Functions by Linear Difference Equations. In Advances in Difference Equations (Veszprém, 1995), S. Elaydi, I. Győri, and G. Ladas (Eds.), pp. 213–243.
  • V. I. Gromak and N. A. Lukaševič (1982) Special classes of solutions of Painlevé equations. Differ. Uravn. 18 (3), pp. 419–429 (Russian).
  • V. I. Gromak (1975) Theory of Painlevé’s equations. Differ. Uravn. 11 (11), pp. 373–376 (Russian).
  • V. I. Gromak (1976) The solutions of Painlevé’s fifth equation. Differ. Uravn. 12 (4), pp. 740–742 (Russian).
  • V. I. Gromak (1978) One-parameter systems of solutions of Painlevé equations. Differ. Uravn. 14 (12), pp. 2131–2135 (Russian).
  • 23: 2.11 Remainder Terms; Stokes Phenomenon
    Two different asymptotic expansions in terms of elementary functions, (2.11.6) and (2.11.7), are available for the generalized exponential integral in the sector 1 2 π < ph z < 3 2 π . …
    §2.11(v) Exponentially-Improved Expansions (continued)
    For second-order differential equations, see Olde Daalhuis and Olver (1995a), Olde Daalhuis (1995, 1996), and Murphy and Wood (1997). …
    24: 2.7 Differential Equations
    §2.7(ii) Irregular Singularities of Rank 1
    See §2.11(v) for other examples. …
    §2.7(iii) Liouville–Green (WKBJ) Approximation
    For irregular singularities of nonclassifiable rank, a powerful tool for finding the asymptotic behavior of solutions, complete with error bounds, is as follows: …
    §2.7(iv) Numerically Satisfactory Solutions
    25: 30.8 Expansions in Series of Ferrers Functions
    30.8.1 𝖯𝗌 n m ( x , γ 2 ) = k = R ( 1 ) k a n , k m ( γ 2 ) 𝖯 n + 2 k m ( x ) ,
    Then the set of coefficients a n , k m ( γ 2 ) , k = R , R + 1 , R + 2 , is the solution of the difference equation
    30.8.4 A k f k 1 + ( B k λ n m ( γ 2 ) ) f k + C k f k + 1 = 0 ,
    30.8.9 𝖰𝗌 n m ( x , γ 2 ) = k = N 1 ( 1 ) k a n , k m ( γ 2 ) 𝖯 n + 2 k m ( x ) + k = N ( 1 ) k a n , k m ( γ 2 ) 𝖰 n + 2 k m ( x ) ,
    The set of coefficients a n , k m ( γ 2 ) , k = N 1 , N 2 , , is the recessive solution of (30.8.4) as k that is normalized by …
    26: Bibliography F
  • B. R. Fabijonas, D. W. Lozier, and F. W. J. Olver (2004) Computation of complex Airy functions and their zeros using asymptotics and the differential equation. ACM Trans. Math. Software 30 (4), pp. 471–490.
  • A. S. Fokas and M. J. Ablowitz (1982) On a unified approach to transformations and elementary solutions of Painlevé equations. J. Math. Phys. 23 (11), pp. 2033–2042.
  • A. S. Fokas and Y. C. Yortsos (1981) The transformation properties of the sixth Painlevé equation and one-parameter families of solutions. Lett. Nuovo Cimento (2) 30 (17), pp. 539–544.
  • T. Fort (1948) Finite Differences and Difference Equations in the Real Domain. Clarendon Press, Oxford.
  • F. N. Fritsch, R. E. Shafer, and W. P. Crowley (1973) Solution of the transcendental equation w e w = x . Comm. ACM 16 (2), pp. 123–124.
  • 27: 28.4 Fourier Series
    §28.4(vi) Behavior for Small q
    §28.4(vii) Asymptotic Forms for Large m
    28.4.25 A 2 m + 1 2 n + 1 ( q ) A 1 2 n + 1 ( q ) = ( 1 ) m + 1 ( ( 1 2 ) m + 1 ) 2 ( q 4 ) m + 1 2 ( 1 + O ( m 1 ) ) w II ( 1 2 π ; a 2 n + 1 ( q ) , q ) ,
    28.4.27 B 2 m 2 n + 2 ( q ) B 2 2 n + 2 ( q ) = ( 1 ) m ( m ! ) 2 ( q 4 ) m q π ( 1 + O ( m 1 ) ) w I ( 1 2 π ; b 2 n + 2 ( q ) , q ) .
    For the basic solutions w I and w II see §28.2(ii).
    28: 36.5 Stokes Sets
    The Stokes set takes different forms for z = 0 , z < 0 , and z > 0 . … where u satisfies the equationThe first sheet corresponds to x < 0 and is generated as a solution of Equations (36.5.6)–(36.5.9). …For | Y | > Y 1 the second sheet is generated by a second solution of (36.5.6)–(36.5.9), and for | Y | < Y 1 it is generated by the roots of the polynomial equationHere u is the root of the equation
    29: Bibliography D
  • A. Debosscher (1998) Unification of one-dimensional Fokker-Planck equations beyond hypergeometrics: Factorizer solution method and eigenvalue schemes. Phys. Rev. E (3) 57 (1), pp. 252–275.
  • T. M. Dunster (1990b) Uniform asymptotic solutions of second-order linear differential equations having a double pole with complex exponent and a coalescing turning point. SIAM J. Math. Anal. 21 (6), pp. 1594–1618.
  • T. M. Dunster (1994b) Uniform asymptotic solutions of second-order linear differential equations having a simple pole and a coalescing turning point in the complex plane. SIAM J. Math. Anal. 25 (2), pp. 322–353.
  • T. M. Dunster (1996a) Asymptotic solutions of second-order linear differential equations having almost coalescent turning points, with an application to the incomplete gamma function. Proc. Roy. Soc. London Ser. A 452, pp. 1331–1349.
  • T. M. Dunster (1996c) Error bounds for exponentially improved asymptotic solutions of ordinary differential equations having irregular singularities of rank one. Methods Appl. Anal. 3 (1), pp. 109–134.
  • 30: Bibliography R
  • W. H. Reid (1972) Composite approximations to the solutions of the Orr-Sommerfeld equation. Studies in Appl. Math. 51, pp. 341–368.
  • W. H. Reid (1974a) Uniform asymptotic approximations to the solutions of the Orr-Sommerfeld equation. I. Plane Couette flow. Studies in Appl. Math. 53, pp. 91–110.
  • W. H. Reid (1974b) Uniform asymptotic approximations to the solutions of the Orr-Sommerfeld equation. II. The general theory. Studies in Appl. Math. 53, pp. 217–224.
  • È. Ya. Riekstynš (1991) Asymptotics and Bounds of the Roots of Equations (Russian). Zinatne, Riga.
  • G. M. Roper (1951) Some Applications of the Lamé Function Solutions of the Linearised Supersonic Flow Equations. Technical Reports and Memoranda Technical Report 2865, Aeronautical Research Council (Great Britain).