06.09.2021 Views

Basics of Fluid Mechanics, 2014a

Basics of Fluid Mechanics, 2014a

Basics of Fluid Mechanics, 2014a

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

5.5. EXAMPLES FOR MASS CONSERVATION 161<br />

(1)<br />

(2)<br />

U 0<br />

Edge <strong>of</strong> Boundry Layer<br />

L<br />

Fig. -5.7. Boundary Layer control mass.<br />

Example 5.6:<br />

Experiments have shown that a layer <strong>of</strong> liquid that attached itself to the surface and it<br />

is referred to as boundary layer. The assumption is that fluid attaches itself to surface.<br />

The slowed liquid is slowing the layer above it. The boundary layer is growing with x<br />

because the boundary effect is penetrating further into fluid. A common boundary layer<br />

analysis uses the Reynolds transform theorem. In this case, calculate the relationship<br />

<strong>of</strong> the mass transfer across the control volume. For simplicity assume slowed fluid has<br />

a linear velocity pr<strong>of</strong>ile. Then assume parabolic velocity pr<strong>of</strong>ile as<br />

[ y<br />

U x (y) =2U 0<br />

δ + 1 ( y<br />

) ] 2<br />

2 δ<br />

and calculate the mass transfer across the control volume. Compare the two different<br />

velocity pr<strong>of</strong>iles affecting on the mass transfer.<br />

Solution<br />

Assuming the velocity pr<strong>of</strong>ile is linear thus, (to satisfy the boundary condition) it will<br />

be<br />

U x (y) = U 0 y<br />

δ<br />

The chosen control volume is rectangular <strong>of</strong> L × δ. Where δ is the height <strong>of</strong> the<br />

boundary layer at exit point <strong>of</strong> the flow as shown in Figure 5.7. The control volume has<br />

three surfaces that mass can cross, the left, right, and upper. No mass can cross the<br />

lower surface (solid boundary). The situation is steady state and thus using equation<br />

(5.13) results in<br />

x direction<br />

{ }} {<br />

in<br />

out<br />

{ }} { { }} {<br />

∫ δ ∫ δ<br />

U 0 y<br />

U 0 dy − dy =<br />

δ<br />

0<br />

0<br />

y direction<br />

{ }} {<br />

∫ L<br />

0<br />

Uxdx<br />

It can be noticed that the convention used in this chapter <strong>of</strong> “in” as negative is not<br />

“followed.” The integral simply multiply by negative one. The above integrals on the

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!