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Boundary Lyer Theory

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CHAPTER I V<br />

General properties of the Navier-Stakes equations<br />

Reforc pssing on to thc int,rgrat,inn of the Navitx-Stokrs cqunl.ions in the<br />

following ch:lpt,ers, it now sncms pcrtincnt, to discnss some of their general properties.<br />

In doing so wc shsll restrict ollrsclvcs to irrcornprcssiblc viscous fluitls.<br />

R. J)c.rivntion nf Reynolds's principle of sindnrity from the<br />

Nnvicr-Stokes cquntiorla<br />

TJr~til I,Ilc prrscnt day no gcncd a.nn.lyt,ic n~rthotl.s 11:tvr I~rcotnc availnblc for the<br />

intc-gmtion of t,hc Navirr-Sl.okcs~cl~~at~ions. I~urtl~crmorc, soluLion~ wl~inh arr vnlitl<br />

for all values of viscosity are Irnown only for some particular cases, c. g. for Poiseuille<br />

flow through a circular pipe, or for Couctte flow bet,ween two parallcl walls,<br />

onc of which is at mst,, the other moving along its own plane with a constant<br />

velocity (set: Fig. 1.1). For this reason tl~c problcm of calculatir~g the motion of<br />

a viscous fluitl was attaclrctl by first tackling limiting cases, that is, by solving prohlcrns<br />

for very large viscosit,ics, on the one hand, and for very small viscosities on<br />

the other, I)cmusr in t,ltis manner thc matllcmatical problem is considerably simpli-<br />

Actl. liowevrr, tho casr of modcratc viscosit,ics cannot be intmpolatd I~ct~ween<br />

thsc two rxtrornes<br />

1l:ven the limit,ing cases of vcry largc antl very small viscosities present great<br />

mat,hemntical tlifficulties so that rescarch into viscous fluid motion proceedetl<br />

to a largc cxtcnt. by experiment. In this conncxion t,hc Navier-Stnlrcs equations<br />

furnish vcry uscSul hints which point to a considerable rcduct,ion in the qnantity<br />

of cxperimcntal work required. It is ofhn possible to carry out. expcrimcnts on<br />

models, which means that in the experimental arrangement a geometrically similar<br />

model of tho aot11a1 body, but reduced in scale, is investigated in a wid tunnel,<br />

or other s~ritahlc arrangement. This always raises the question of the dynamic<br />

sim~ilnril?y of fluid mot.ions which is, evidcnt.ly, intimately connectmi with the question<br />

of how far rcsult.~ obta.inod wit,h motlcls can Jlc ntilizcd for the prediction of<br />

tho Id~aviour of the full-scale body.<br />

As alrr:dy oxpl~incrl in Chap. I, two fluitl nibtions are dynamically similar if,<br />

with gc?ornct,rit:ally sirnilnr k)oundn,ries, the velocity ficltls are geometrically similar,<br />

i. e., .if t1tc.v have gromctricnlly similar strcnrnlincs.<br />

This question was answcrrd in Chap. 1 for thr caw in which only inertia and<br />

visrntts fnrt~s t:~Itc pitrl. in the process. It was found there that for the two motions<br />

I<br />

the RrynoItIs IIII~I~JC~S mnst be rqunl (lirynolcls's pri~~~i~)lcb of sirnil:~rit.y). 'I'his<br />

roncllrsion was drawn by astimating thc forces in the strewn; wr now propose to<br />

tlctlr~ce it again directly from thc Navicr-Stolrcs equations.<br />

'rlrc Navicr-Stokes cqr1a1,ions cxpress tho condition of cqt~ilil>ri~~~~t,<br />

II:IIIICI~<br />

that for cnc11 pa.rticle thrc is eqrrilibriurn betwccn hly forcrs (woigI~(.), SII~~;LC~<br />

for~cs a~ttl jncrti:~. forcrs. 'J'hc sr~rfac!c forc:c:s co11sist. of prcwurr for(*c.s (IIO~~II:~~ Ii)r(:(:s)<br />

and frictiotl forrcs (sl1ea.r forccs). TZotljr forccs n.rc in~port,nt~t, only irl c::t.sc>s ~IIC:II<br />

tlicro is a free s~~rfncc or whcrl l,lto tlrtlsily clisl.ril~trl.ion is it~l~orno~c:~~c:o~ts. III 111,:<br />

(:xs~ of a hornogcnrol~s fl~titl in tltc :l.hscnc:t? oS n Srrc wtrfi~cc tltrrc is c:(l~tiIiI)t.i~tt~~<br />

l~ctwc(~t tho wcigltb of'c:at:l~ p;~.rl.ivlc at111 it,u I~.yrlrwld,iv I )IIO.~IIII~:~ l'orc;~!, in tl~c S:I,IIIC<br />

w:~y 3.8 at rost. Ilc:nco in 1.11~ rnot,iorl of a I~o~nogcncons Illticl, ir~ thc nt~sct~c:c of:^ I'rrc?<br />

snrf:icc, body forces can 11r canrcllctl if prcssttrc is t,dt~n to IIIC:II~ tho (Iillcr~~ncc<br />

I~ctwccn that in n~ot,ion a.nd at rcst. In t h following arpttnc~tt, wc sl~nll rc.st,ric:t. our<br />

at,tc~~tion to cases for whic:h this assttn~ption is trtrc bccalisc they arc t,ltc: tnost imporhnt<br />

oncs in n.pplicntions. Tltr~s bltc Nnvicr-Stoltcs rqnations will now c:ortt,air~<br />

only forces clue to pressure, viscosity, and inertia.<br />

Unclor thwc assumptions and ronvcntions ihc N~~vicr-Stolccs rqn:ttions for<br />

:In inromprcssiblc fluid, rcstrick:tl 10 stci~dy llow nncl in vcclor fnrttt, sinl1~lil:y to<br />

This clifl'crential equation must he indrpcnclent d the clloicc of the utli(.s for t.lrc<br />

various physical quantities, suc:h as velocity, prcssnrc, clc., which appe:lr in it.<br />

We now consider flows about two gcomctrically similar boclics of diKcrcnt lincar<br />

tlimcnsions in streams of different velocitics, c. g., flows past two spt~cms in wllictl<br />

the densitics and viscosities may also bc different. Wc shall invcstigatc the condition<br />

for dynamic similaritfly with the aid of tho Navier-Stokcs cquat,iot~s. Evidently,<br />

dynamic similarity will prevail if with a suitablc choice of the units of Icngf.h,<br />

tirnc, antl force, the Navicr-Stokes cqn. (4.1) is so tmnsforn~ctl that it, I)ccomcs<br />

identical for the two flows with geomctric:ally similar botir~tlarics. Now, it is [~ossiblc:<br />

to free oneself from the fortuitously selechcl units if clirncnsiorllcss q~~ntltitics n.rc<br />

introduced into cqn. (4.1). This is achievctl by snlcct.ing ccrt,:~in suitnhlc c:har:rt:taristic<br />

mxgnitudcs in thc flow as our ~rrtil,s, antl by refixring all otlwrs t,o t11c:nr.<br />

., .Ll~us c. g., thc frcc-slrcarn vcloci1,y anrltl tllc tlianlcl.cr of Ll~r sphrrc: cnlt IJC srl(:c:t.t:tl<br />

as the rcspcctivc 11ni1.s of vcloc:it.y and Icngth.<br />

1~r.t V, 1, and pl clcnotc tl~csc characteristic rcfcrcnco magt:itrltlrs. II' we now<br />

introtltlcc into thc Navicr-Sl.okcs oqn. (4.1) thc tlirrrrnsionlrss ri~tios

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