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►See Armitage (1989), Berry and Keating (1998, 1999), Keating (1993, 1999), and Sarnak (1999).
►The zeta function arises in the calculation of the partition function of ideal quantum gases (both Bose–Einstein and Fermi–Dirac cases), and it determines the critical gas temperature and density for the Bose–Einstein condensation phasetransition in a dilute gas (Lifshitz and Pitaevskiĭ (1980)).
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Sidebar 21.SB2: A two-phase solution of the
Kadomtsev–Petviashvili equation (21.9.3)
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►A two-phase solution of the Kadomtsev–Petviashvili equation (21.9.3).
Such a solution is given in terms of a Riemann theta function with two phases.
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►In both the modulus and phase of the asymptotic variable need to be taken into account.
…Then numerical accuracy will disintegrate as the boundary rays , are approached.
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►In the transition through , changes very rapidly, but smoothly, from one form to the other; compare the graph of its modulus in Figure 2.11.1 in the case .
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►uniformly with respect to in each case.
►The relevant Stokes lines are for , and for .
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Go. Torres-Vega, J. D. Morales-Guzmán, and A. Zúñiga-Segundo (1998)Special functions in phase space: Mathieu functions.
J. Phys. A31 (31), pp. 6725–6739.
S. A. Tumarkin (1959)Asymptotic solution of a linear nonhomogeneous second order differential equation with a transition point and its application to the computations of toroidal shells and propeller blades.
J. Appl. Math. Mech.23, pp. 1549–1565.
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►The zeros in Table 36.7.1 are points in the plane, where is undetermined.
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►The zeros are lines in space where is undetermined.
…, ), the number of rings in the th row, measured from the origin and before the transition to hairpins, is given by
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►In Figure 36.3.13(a) points of confluence of phase contours are zeros of ; similarly for other contour plots in this subsection.
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Figure 36.3.13: Phase of Pearcey integral .
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Figure 36.3.14: Density plots of phase of swallowtail canonical integrals.
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Figure 36.3.21: Phase of hyperbolic umbilic canonical integral .
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►These examples of transitions to turbulence are presented in detail in Drazin and Reid (1981) with the problem of hydrodynamic stability.
The investigation of the transition between subsonic and supersonic of a two-dimensional gas flow leads to the Euler–Tricomi equation (Landau and Lifshitz (1987)).
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