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Boundary Lyer Theory

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4GO XVI. Origin of turbulence 1 1). Principles of the theory or stnbility of Inrninnr flows 4G1<br />

JIerc c, t1cnot.c~ the vclocit,y of propaption of t,hc wave in the z-dircction (phase<br />

vclooity) wl~crcas c, again dcLertnincs t,ho tlcgrce of damping, or nmplificntion, ticpending<br />

011 it,s sign. I'hc arnplit,~~tle function, 4, of the flnct,tlation is ass~~~nccl to tlcpcntl<br />

on y only ~C(:ILIISC the mcm Ilow tlcpcnds on y alone. I'roni cqn. (16.10) it is possible<br />

to ol)t,ain 1.11r c:ornponcnlss of thr: pcrt,rrrl)nt.ion vcloc:it,y<br />

11,' -<br />

t)l/,<br />

-<br />

i)y<br />

: ,#,'(?/) (.""' PI' , (10.12)<br />

1) -=<br />

Ry1 --<br />

ax<br />

i u +(?I) &my PI) .<br />

Irlt.rotl~tc:ir~g I,l~c:sc- valnrs inh rqns. (16.7) and (10.8), we obtain, after the elirninat.io11<br />

of prrssnrc, l11c following, ordinary, fourth-order, differential cquation for the<br />

n.tnl)litwlc 4(y) :<br />

I<br />

When the mean flow IJ (11) is specified, eqn. (IF. 14) contains four pamrnnt.rrs, n :~n~cl~ a,<br />

R, c, anti c,. Of t.hcse the rtcynoltls nrlml)or of the moau flow is liltcwiso spccill(:d<br />

and, f~~rthcr, the ~avcl~ngth i = 2 n/a of the disturb:m(:c is to bc consitlcrctl given.<br />

In t.his rase the differentid equation (IF.l4), togcthrr with thc Imlntlary c:ontlitiorrs<br />

(16.15), f\rrnish one oigrnf'uncLion +(?I) and one complex cigcnv:~ll~r: c == c, 1 i ci<br />

for (wh pir ol' v:~l~tt.s a, R. I Ivrc cr rt:~~rcsw~l~s I,IIc ~)II:LSC v(hwiI,.y 01- 1.11~ l~rw(:ril~t:~l<br />

t1isturbnncc wltcrcas thc sign of c, tlcLcrnlit~cs wllctllrr bho wave is amptilictl (ci :.O)<br />

or tla.tnpctl (ci < O )t. For c, < 0 the correspontling flow (IJ, R) is stnth for lllc ~ivcn<br />

valur of a, wllcrrns c, > 0 tl~notcs il~stabilit~y. Thc limiling case c, - 0 corrrsponds<br />

1.0 nrnLml (indiKcrmt) dist~rrl~ancrs.<br />

11nm1)cr is the critical Reytrolds nuinher or limit<br />

of Ian~inar flow untlcr cot~sitlcrxLion.<br />

Fig. 16.8. Curves of neutral stabi1it.y for<br />

two-di~nensionnl borlntlary layer wi(.tr<br />

two-dimensional disltlrbrmccs<br />

(a) "non-visrolls" inslal,ilily; in thc rnsc nC vclocity<br />

~~rnillrs or 1yp :t wilh pin1 *d i~~flrxion<br />

PI, thr rllrrc or 1w111rnl slnbility is or typc :,<br />

(1,) "visrow" Instahllity; in I11e raw or vriorit,)<br />

proIllrr nl type 8 uilhotrt poi111 of lnflrxion, llw<br />

rurve ol erutml shbilily is or lypc b<br />

Tl~n nryrnglotm Tor ll~n rrlrvc or rwulral stnbility<br />

a al. R --+ r, arc ohlxincd rroln llw "rrirlionlrar"<br />

slal~ilit?. rrlllalio~i (16.16)<br />

r ,<br />

I he rxprritnrntd rvi(Irncr eonwrnit~g t,ransit,iot~ fro111 l:~n~in:t,r 1-0 I,II~I~~III~II~,<br />

flow rcfrrrrtl 1.0 ~)roviorlsly I(.nds 11s t,o cs~~rcl, that, ;LI, SIII:LII Ib(~,y~~oI~ls I I I I I I I I ~ for ~ ~<br />

wl1ic.11 I:~minar llow is ol~servrtl. all \v:rvrl~ngt.l~s wo~lltl l)rorluc*v ot~lg sl.:rl)lr tlist.llrl):~l~c~s,<br />

wl~rrrn.s :lip I:~r.gt-r ltc!g~~oltls rtlln~l)rrs, li~r wllic~l~ I.II~IIIII~:III, IIow is 011svr\~1~1,<br />

ul~st,:~l)lc tlist~lirbarlccs o~tght, t,o corrcs~~ontl to at, I(ywt, sonto \v:Lv~I~II~~.IIs. IIo\r.(:v(~,<br />

it is nwrssnry t,o rcn~nrk at tallis poitlt t.l~:rt~ t.11~ vrit,ic:n.l I

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