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If velocity distribution, u in laminar boundary layer over a flat plate is assumed to be given by second order polynomial

u-a+by-cy”, where y is the perpendicolar distance measured from the surface of the flat plate and a, b and c are constants. Determine the expression of velocity distribution in dimensionless form as =(yδ) where, U is main stream velocity at boundary layer thickness δ. Further also find boundary layer thickness in terms of Reynolds number.

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Velocity distribution: u=a+bycy2

The following condition must be satisfied:

i)At y=0 , u=0

∴u=a+bycy2

0=a+0-0 ∴a=0

ii)At y=δ, u=U

∴U=bδcδ2………………………(i)

iii)At y=δ,dudy=0

(dudy)(y=δ)=ddy(a+bycy2)=b2cy=b2cδ=0…………(ii)

Substituting values of b=2cδ from (ii) in (i), we get

U=2cδ2cδ2

U=cδ2

c=Uδ2

Hence from the velocity distrubution is:

u=2Uδδ2yUδ2y2

$u=\frac{2U}{δ y}-\frac{U}{δ^2} …

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