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Boundary Lyer Theory

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630<br />

XVII. Origin ot t.~~rhr~lrncc J l<br />

This ineqnnlity contnins Rayleigh's criterion from eqn. (17.19) as a special case<br />

ant1 rcs~~lt.s wherl 7o = 0 is ns~nmcd here; we then find that 1 + 5 > 0. The stability<br />

calcnlntion which led to eqn. (17.23) took into account disturbances which were<br />

not ~icccssnrily axially symmetric; the 1n.th.x turned out, to be the "moat dangerous"<br />

oms ant1 detcrminctl (he litnit of st.:~l)ilil.y implied by thc ineqrlnlity (17.23). l'ignro<br />

17.36 shows an example of an unstable flow which contains vortices in the shape<br />

of spirals. If. Ludwirg's tllcory has bccn compared withexpcrirnent.al resulk [134]<br />

in Fig. 17.36. Every bnse flow invcstigated experimentally is represented by a point<br />

in t,Ilc I;, 271 plane. The opcn ant1 full circles characterize stable and unstable flow,<br />

respectivciy, it being riotcd that vortkcs were observed for the latter. It is seen<br />

t.hn.t, IT. I,utlwicg's st.:~l)ilil.y crit,crion from rqn. (17.23) is fully confirmed hy cx-<br />

Fig. 17.37. R.nngen of Inwinnr nnd l,rrrl)~tlet~t, flow in n~~tii~luu I~C~IYC~II two concctltric. cyli11tlc.r~;<br />

innrr cylinricr rotntrs. outm cylitldrr nt. rn~I, in prmRltro of nxi:d flow: plot. in t.crr~lu of 'l'r~~lor IIII~II.<br />

I,t.rT,, 1111rl IIIIIIII#('). R.,; tlll~ll~11~l~llll'l1(H 1))' #I. I

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