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da] be less than the circumference; but unstable if [lambda] be greater than the circumference of the cylinder. Disturbances of the former kind lead to _vibrations_ of harmonic type, whose amplitudes always remain small; but disturbances, whose wave-length exceeds the circumference, result in a greater and greater departure from the cylindrical figure. The analytical expression for the motion in the latter case involves exponential terms, one of which (except in case of a particular relation between the initial displacements and velocities) increases rapidly, being equally multiplied in equal times. The coefficient (q) of the time in the exponential term (e^{qt}) may be considered to measure the degree of dynamical instability; its reciprocal 1/q is the time in which the disturbance is multiplied in the ratio 1 : e. The degree of instability, as measured by q, is not to be determined from statical considerations only; otherwise there would be no limit to the increasing efficiency of the longer wave-lengths. The joint operation of superficial tension and _inertia_ in fixing the wave-length of maximum instability was first considered by Lord Rayleigh in a paper (_Math. Soc. Proc._, November 1878) on the "Instability of Jets." It appears that the value of q may be expressed in the form / / T \ q = / ( -------- ).F(ka), (2) \/ \[rho]a^3/ where, as before, T is the superficial tension, [rho] the density, and F is given by the following table: -- +--------+--------+--------+--------+ | k^2a^2.| F(ka). | k^2a^2.| F(ka). | +--------+--------+--------+--------+ | .05 | .1536 | .4 | .3382 | | .1 | .2108 | .5 | .3432 | | .2 | .2794 | .6 | .3344 | | .3 | .3182 | .8 | .2701 | | | | .9 | .2015 | +--------+--------+--------+--------+ The greatest value of F thus corresponds, not to a zero value of k^2a^2, but approximately to k^2a^2 = .4858, or to [lambda] = 4.508 X 2a. Hence the maximum instability occurs when the wave-length of disturbance is about half as great again as that at which instability first commences. Taking for water, in C.G.S. units, T = 81, [rho] = 1, we get for the case of maximum instability a^(3/2) q_(-1) = --------- = .115d^(3/2) (3), 81 X .343 if d be the diameter of the cylinder. Thus, if d = 1, q^(-1) = .115; or for a diameter of one centimetre the d
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