Variables of interest for steady uniform flow are: (1) the mean velocity V, (2) the discharge Q,

(3) the velocity distribution v(y) in the vertical, (4) the head loss HL through the reach, and (5) the

shear stress, both local τ and at the bed τo. These variables are interrelated.

Shear stress τ is the internal fluid stress which resists deformation. The shear stress exists only

when fluids are in motion. It is a tangential stress in contrast to pressure, which is a normal

stress.

The local shear stress at the interface between the boundary and the fluid can be determined

quite easily if the boundary is hydraulically smooth; that is, if the roughness at the boundary is

submerged in a viscous sublayer as shown in Figure 2.7.

Figure 2.7. Hydraulically smooth boundary.

Here, the thickness of the laminar sublayer is denoted δ′. In laminar flow, the shear stress at the

boundary is:

dv

τ o = at y = 0

(2.66)

dy

The velocity gradient is evaluated at the boundary. The dynamic viscosity is the proportionality

constant relating boundary shear and velocity gradient in the viscous sublayer.

When the boundary is hydraulically rough, the thickness of the laminar sublayer is very small

compared to the roughness height. The paths of fluid particles in the vicinity of the boundary are

shown in Figure 2.8.

The velocity at a point near the boundary fluctuates randomly about a mean value. The random

fluctuation in velocity characterizes turbulent flows. As shown in Figure 2.9a, the particle has a

vertical component of velocity vy as well as a horizontal component vx.

2.16

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