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Boundary Lyer Theory

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754 XXJV. Frce turhnlent flows; jets and wakes Rcfcrenccs 755<br />

Exp. I1<br />

1.36<br />

0 2.34<br />

0 3.65<br />

A 1.19<br />

A 2-01<br />

Fig. 24.12. The mixing of coaxial turbulent jets<br />

of different velocities and temperatures in a pipe,<br />

after S. R. Ahmcd [la]. Variations of the velocity<br />

along the nxis of the pipe n) for vnrious velocity<br />

rntios U* = urro/~so at a constant value of the<br />

temperature rntio O*; b) for vnrioua values of t.lie<br />

temperature ratio Q* = Olro/Oso at a constant<br />

value of the velocity. F* = frro/fso denotes the<br />

area ratio of the inner jet Lo the whole jet<br />

two cases: 1, two-dimensional [low above a lincar source of heat placed on a horizont,nl<br />

floor and 2. &xi-symmetrical flow above a point-source. In both cases the width of<br />

the velocity and temperatmure profilc increases in clircct proportion to the height<br />

abovc the floor, x. In the two-dimensional cnsc thc vcloait-y rcmains constant at dl<br />

heighbs, whereas the temperalure dccreeses as x-1. In thc axially symn~etrical casc<br />

the velocity is proportional to 2-113, the temperature being proportional to x-514.<br />

The two-dimensional case was treated theoretically on the basis of Prantltl's mixing-<br />

length theory (tmnsport of rnomcntum) as well as on thc basis of G. I. Taylor's<br />

vorticity tmnsport tlteory. The nxially ~ymmctricnl casc could bc invcst~igntcd only<br />

with the aid of Prandtl's thory bccausc G. I. Taylor's tlicory brcnlts clown in thig<br />

case. Measurements performed for thc axi-syn~met~rical enso conf rm t.11~ thcorrl~ical<br />

cslculations. The diffusion of temperature behind a point-source and behind n Linear<br />

source placed in the boundary layer on a flat plat,c were investigated experi~ucntslly<br />

by I

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