written 5.7 years ago by |
Velocity distribution in smooth pipes
$u=\dfrac{u_*}{K}\log_e y+C$
It is seen that at (y=0), the velocity ‘u’ at wall is ($-\infty$).
This means ‘u’ is positive at some distance far from the wall.
Hence, at some finite distance from wall, (‘u’=0).
Let the distance from pipe wall b y’. Now, constant C is determined from the boundary condition, i.e., at (y=y’), (u’=0),
$\therefore 0=\dfrac{u_*}K\log_e y’+C$
$\therefore C=-\dfrac{u_*}K\log_e y’$
Putting the value of ‘C’ in the above equation, we get
$\therefore u=\dfrac{u_*}K\log_e y-\dfrac{u_*}K\log_e y’$
$\therefore u=\dfrac{u_*}K\log_e \left(\dfrac y{y’}\right)$
Substituting the value of K = 0.4, we get
$\therefore u=\dfrac{u_*}{0.4}\log_e \left(\dfrac y{y’}\right)$
$\therefore u=2.5 u_*\log_e \left(\dfrac y{y’}\right)$
$\therefore \dfrac u{u_*}=2.5 \times2.3\log_{10} \left(\dfrac y{y’}\right)$
$\left[\because \log_e \left(\dfrac y{y’}\right)= 2.3\log_{10} \left(\dfrac y{y’}\right)\right]$
$\therefore \dfrac u{u_*}=5.75\log_{10} \left(\dfrac y{y’}\right)………………(1)$
For smooth boundary, there exist a laminar sub-layer.
The velocity distribution in laminar sub-layer is parabolic in nature.
Thus, in laminar sub-layer, velocity distribution does not hold.
Therefore assume y’ proportional to $\delta'$
$\therefore y’=\dfrac {\delta'}{107}$
Where, $\delta'=\dfrac{11.6v}{u_*}$, where v = kinematic viscosity.
$\therefore y’=\dfrac {\dfrac{11.6v}{u_*}}{107}$
$\therefore y’=\dfrac {0.108v}{u_*}$
Substituting this value in equation (1), we get
$\therefore \dfrac u{u_*}=5.75\log_{10} \left(\dfrac y{\dfrac {0.108v}{u_*}}\right)$
$\dfrac u{u_*}=5.75\log_{10} \left(\dfrac {yu_*}{0.108v}\right)$
$\dfrac u{u_*}=5.75\log_{10} \left(\dfrac {yu_*}{v}\times9.259\right)$
$\dfrac u{u_*}=5.75\log_{10} \left(\dfrac {yu_*}{v}\right)+ 5.75\log_{10}(9.259)$
$\dfrac u{u_*}=5.75\log_{10} \left(\dfrac {yu_*}{v}\right)+ 5.55…………..(2)$
Velocity distribution in rough pipes:-
In case of rough boundaries, the thickness of laminar sub-layer is very small.
The surface irregularities are above the laminar sub-layer, hence the laminar sub-layer is completely destroyed.
Therefore y’ is proportional to ‘K’.
$\therefore y’=\dfrac {K}{30}$
Substituting this value of y’ from equation $\left[ \dfrac u{u_*}=5.75\log_{10} \left(\dfrac y{y’}\right)\right]$ , we get
$\dfrac u{u_*}=5.75\log_{10} \left(\dfrac y{\dfrac {K}{30}}\right)$
$\dfrac u{u_*}=5.75\log_{10} \left(\dfrac {y}{K}\times30\right)$
$\dfrac u{u_*}=5.75\log_{10} \left(\dfrac {y}{K}\right)+ 5.75\log_{10}(30.0)$
$\dfrac u{u_*}=5.75\log_{10} \left(\dfrac {y}{K}\right)+ 8.5…………..(3)$