Environmental Engineering Reference
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2002). Similarly, the perturbation equation along the C2-family of characteristic curves is
§
W
U
·
d
(
''
u
(2
(
gh
) ))
' ¨
0
¹
(4.A11)
¸
d
t
h
©
m
In a steady laminar flow of a Bingham fluid, the shear stress W 0 is given by (4.A1):
(4.A12)
Figure 4.A1 shows the general velocity distribution of Bingham flow in an open channel. The upper
part is a plug in which the fluid flows at a uniform velocity u p , which is nearly equal to the average
velocity. Only in the zone near the bed does the velocity vary, from zero to u p . The thickness of the layer
is assumed to be į . The velocity gradient, therefore, is roughly u / į , and
W W H
0
B
§
·
d
W
u
B
¹
(4.A13)
(
''
u
(2
gh
))
'
K
¨
¸
d
t
U
h
UG
h
©
m
m
Fig. 4.A1 Velocity distribution of non-Newtonian open channel flow for a Bingham fluid
As shown in Fig. 4.A2, a perturbation that occurs at point A ( x , t ) in the x - t plane will propagate along
the characteristic curves AB and AC . For any point B on the C 1 1 characteristic curve that passes through
the point A ( x , t ), a characteristic curve C 2 2 intersects the C 1 1 curve at point B . There is a relation between
' u and
at point B (i. e. any point on the C 1 1 characteristic curve).
'
(2 (
gh
) )
Fig. 4.A2 Characteristic curves on the x - t plane (The abscissa is the x -axis and the ordinate is the time t -axis). If a
perturbation occurs at the point A , it propagates downstream along the C 1 1 curve and upstream along the C 2 1 curve
The area below the curves CAB is undisturbed. The initial perturbation has no effect on the area, and the
velocity u and depth h remain constant. Integration of Eq. (4.A11) along the C 2 2 characteristic curve yields
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