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Boundary Lyer Theory

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114 VI. Vcry slow motion<br />

where r2 = z2 + y2 4- z2 has been introdneed for the sake of brevit,y. Tt, is easy to<br />

verify that these expressions satisfy eqns. (6.3) and (6.4) and that t.ho velocity va-<br />

ninhes at all pointa on the surfnco of t,ho sphere. The pressure on t,he surfnre becomes<br />

'rho rnnximllm ant1 n~inimurn of prrssllrc occurs nt points P, and I'2, respectively,<br />

thrir valnrs bring<br />

3 11 uw<br />

1)1.2- pcn - -1- --ji -<br />

(G 7 1))<br />

Tile prcssnrc distribr~t,ion along a 1ncridia.11 of t,hr sphere as well as alor~g the axis<br />

of al)scissar, r, is shown in Fig. 6.1. '1'11~ shrnring-stress distribution over the sphere<br />

can also be cnln~libtctl from the n.lmvo formulae. If, is found that the shearing st,ress<br />

has it,s largoat value nt poirll /I whcro t = ij ,IL fJ,/I1 :m(I is r~(11al to the pressllre<br />

riso nt PI or prrssurc tlccrrase nt /',. Tntrgmting tho pressure distribut.ion ant1 the<br />

shrnring sl,rrss over the surfacr of tho sphrre we obt,nin t,ho t,ot,nl tlrng<br />

'This is f,ltc vcry wcll known ,Wko.~ cr/udion for thc: tlrag of a spl~rrc. It, can I1v shown<br />

t,l~at. ol~c t.llirtl of ihc t1r:t.g is tlrro t,o the prossure ,list,ril)~ition n ~ ~.II:L~, ~ d tho ron~ni~~ir~g<br />

t.wo t,l~irtls nrr t111o t.o tho cxistctico of shcar. It is fr~rlhar rcrnark:~l)lc t,h:lt t,hc ctr:~g<br />

is ~xo~)~rt,io~~nl to the first, powcr of vclocity. If a t1ra.g coefficient is fornled hy<br />

rc.l;.rrillg f,llc tlr;la 1.0 t,hc tlyu:~mic hc:r.rl a Q 11,2,nntl t.he rrontd arca., :IS is dotlc:<br />

in tllc c.:rsct of highrr Ib~~noI(Is r~n~nlwrs, or if we p~t.<br />

b. Parallel flow pnst 8 spl~rrc 116<br />

A coniparisot~ het,ween Stolzcs's equation nnd rxpcritnont was givan in Vig. 1.6<br />

from which it is seen that is applies only to rases when R < 1. The pnt,tern of<br />

strcamlinos in front of and behind the sphere must be the same, as by rcvvrsing<br />

t,he direction of free flow, i. e., by changing the sign of vclocity con~ponents in cqns.<br />

(6.3) and (6.4) t.he syston~ is transformed into it,self. The st,reamlincs in viscons<br />

flow past. a sphcro are sl~own in Fig. 0.2. Thy were tlrnwn ns they woultl nl)pear<br />

to an observer in front of whom the sphere is dragged with n constnnt, vclocity U,.<br />

The sltrt,ch contains also velocit,y prolilcs at scvcral cross-s~ct~ions. It is scon f,l~nt<br />

tho sphere drags with it a vrry witlr layer of flnitl wl~id~ rxtr~~tls over :iI~out, one<br />

tliitrnclor on I)oth sitlns. At, vory high Itryrtoltls nurnl)ors tl~is I~o~ln~liiry li~y~r<br />

I)ccornes very thin.<br />

Ipig. 6.2. Sl.rcnnilincs nnd vrloci1.y di.st.ri-<br />

brttinr~ in Stokm' snlut.ior1 for n spllcrr ill<br />

pa r;dlrl flow<br />

[Pig. 6.3. S1.rc;itnlirlr.s in llir flow<br />

ORCVII'.~ improvcrnt~~~t: An ~ITI~)~~VI!ITI(-II~, of' St,ok~s's srv is', 11' nntl 711' nrr t,l~o pcrl,url):l (.ion f.cwns, : rr~tl :IS SIIV~I, stn;r ll wit 11 ~.c~sl~~~,,<br />

t.0<br />

(.he f'rcr st,rca~n vclocity (1,. It is to noted, I~owevcr, that, this is r~ot, tr~r ill 1,11c<br />

irnnlrrliatr neighl~onrhootl of t,hc spherr. With tho ns~nnl~~i~iot~ (0.1 I ) 1.111- illrrt.ia<br />

t.crms it) t,hr Na,vier-Stdokt,s rqns. (3.32) arc tlrcv~nl)osed in two ,pro~~l)s, r. g. :<br />

allr av'<br />

(loo , U, --<br />

ax<br />

, . . . and<br />

a ~ ' , avr<br />

"Iaz , IL ax<br />

--, . . .

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