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Boundary Lyer Theory

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142 VII. Hor~nclnry-lnyrr rq~~ntii~t~s for t\vo-di~i~rr~nio~l~~l Ilow; I)o~~nilr~r,y Inyrr on n plelo<br />

Fig. 7.9. Vclocity rlist.ril)~~lion in tho Inn~i~inr hounrlnry lnyrr on n IlnL plntr nt, xrrn i~~rirlrncr.<br />

nn ~ncasr~rcd by Nikr~rndso [20]<br />

I:ij!. 7.10. Lord rocffiricnt<br />

nf 6Izi11 frirtion 011 a flnt,<br />

])l:iln at ZPITJ iriridr~lco in<br />

0.001<br />

i~~con~prcssi blo fln\v, dclcrminc~l<br />

from tlirocl. tncnnnrc-<br />

0 0005<br />

twnt of shearing strcss by 0.0067<br />

O hd~recl skm fiiclioon measurement<br />

fmm velonfy profile<br />

D/recl skin frctlin measuremen/, x - 28 6 cm<br />

0 t r ,x-56cm<br />

- ! I l l l l l l l I 1 I<br />

,.<br />

I ltc laminar law of friclion on :L flat phtc was also subjectctl to careful expcrirncntal<br />

verification. The local shearing stress at the wall can be determined<br />

intiirecthj from the slope of the velocit,y profilc at the wall together with eqn. (7.31).<br />

In rccrnt t,imcs IT. W. Liepmann and S. Dhawan [18] measured the shearing stdress<br />

tlirocI.ly from the forco acting on a small porl,ion of t,ho plnto which wns nrrnngctl<br />

so t,l~at it could move slightly with respccl to the main plate. The results of tl~eir<br />

wry careful measurements arc seen reprotluccd in Fig. 7.10, which shows a plot<br />

of the local coefficient of skin friction cf' -- to/k Q 1Jm2, against, thc R.cynolds<br />

number R, = 11, z/v. In the range of R, = 2 x 10"o 6 x 10"both laminar and<br />

t,urbrrlcnt, flows arc possible. It can be sccn that direct and indircct mcas~~rcmcrtt~s<br />

nrc in cxcrllont agrrorncnt, with each ol,l~or. Mcns~~rcrnonl,~ in tho lnn~innr rnnga give<br />

a strilcing (!o11fit311:kt,io11 of 1Hwius's oqn. (7.X) frm~ which cff .?: 04Wi/d~~. 111<br />

the turl~r~lcnf~ range there is al~o goo(1 ngrecmcnl with I'rntdt.1'~ thcorctif:nl forrnr~l:~<br />

which will bc deduced in Chap. XXI, cqn. (21.12).<br />

r 7<br />

Jllc conlplctc ngrccmcnt bctflwcen t~hrorcticnl and expcrin~cntd rcsr~lt.~ wlliol~<br />

cxist,s for the velocity distribut.ion nncl t,hc shcnring stxcss in a 1aniinn.r honndn.ry<br />

lnyer on s flat plate at zero incidence that, has hcen hrougl~t inta evidcncr in Figs.<br />

7.9 antl 7.10 for the rmge R, > lo5 nnequivocally dcmonstratcs thc valitlity of t,he<br />

bountlnry-ln.yer n.pproximntions from the physicnl point, of vicw. TII spit.(! t,I~is,

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