2.1 KINDS OF OPEN CHANNELS
In general, there are two kinds of open channels: (1) natural, and (2) artificial. Natural channels are formed by Nature through geologic, geomorphologic, and hydrologic action. They include all natural watercourses, from the smallest to the largest. An example of a small watercourse is the small stream or rivulet shown in Fig. 21. An example of a large watercourse is the large river shown in Fig. 22. The largest natural channel is the Amazon river at its mouth, shown in Fig. 23. Applications of openchannel hydraulics in natural streams are typically in the fields of flood control, navigation, and stream restoration.
Artificial channels are also referred to as canals. They are made by humans for a specific purpose, usually to transfer water from a place where it exists in ample supply to a place where it is in short supply, or to transfer water between two locations to satisfy daily, monthly, seasonal, or annual requirements. Artificial channels are also built for flood control and navigation. Artificial canals have been built by ancient societies, usually to transfer water for irrigation or water supply. For instance, Fig. 24 shows a small canal built about 3,500 years ago by the ancient people of Cajamarca, Peru.
Artificial channels can be referred to with various names, depending on their features and intended use:
Uses of Open Channels Open channels, both natural and artificial, are used in various water resources fields, including:
Figure 211 (a) shows an irrigation canal (left) and a drainage canal (right), flowing in opposite directions, in the WelltonMohawk irrigation project, in Wellton, Arizona. The irrigation canal water is being pumped upstream, while the drainage water is flowing downstream.
Figure 211 (b) shows a fishpassage channel at a pondandplug stream restoration site in Ferris Creek, Plumas County, California.
Related Fields Other related fields that benefit directly from open channel hydraulics knowledge include:
2.2 CHANNEL GEOMETRY
Natural channels refer to the great number of streams and rivers around the world. With respect to longitudinal orientation, natural channels are classified as: (a) straight, (b) meandering, or (c) braided. A straight channel is one that follows more or less a straight path. Conversely, a meandering channel curves around in plan view, as shown in Fig. 212. The ratio of stream length to valley length is referred to as sinuosity. The sinuosity of the stream shown is about 5.
A braided channel features multiple interconnected meandering subchannels (Fig. 213). The flow and sediment conditions under which a channel assumes a certain longitudinal shape is a subject of fluvial geomorphology.
During floods, natural channels may overflow their banks and temporarily take up significant portions of the adjacent floodplain (Fig. 214). With respect to flood stage, flow in natural channels is classified as: (1) inbank, when the flow remains in the main channel, or (2) overbank, when the flow spills over to the adjacent floodplains.
Figure 215 shows the typical variation of stage and flood wave travel time K with extent of inundation. These variations are due to relative increases or decreases of surface bottom friction as the stage increases.
Artificial channels are classified as either: (1) prismatic, or (2) nonprismatic. Prismatic channels have a constant cross section, either trapezoidal, rectangular, or triangular. Trapezoidal channels are the most common type (Fig. 216). Rectangular channels are often used in sanitary flows and laboratory applications. Triangular channels are normally used in road and urban drainage.
Nonprismatic channels are those for which the cross section is not constant. Nonprismatic channels are used in the transition from a cross section of one size to another of a different size, usually to account for the variability in bottom slope.
There are three asymptotic crosssectional shapes in prismatic channels (Section 1.3):
A channel is hydraulically wide when the wetted perimeter P can be approximated by the top width T. By definition, the hydraulic radius R is equal to the flow area A divided by the wetted perimeter P. Likewise, the hydraulic depth D is equal to the flow area A divided by the top width T. Therefore, the following relations hold for a hydraulically wide channel:
In practice, a channel may be considered hydraulically wide if the top width T is greater than or equal to 10 times the hydraulic depth D (Chow, 1959):
In general:
in which Q = discharge, A = flow area, and V = mean velocity. Since by definition:
it follows that:
and:
in which q = discharge per unit of channel width, or unitwidth discharge [L^{2} T^{ 1}]. For simplicity, a hydraulically wide channel may be analyzed in terms of its unitwidth discharge. For a hypothetical unitwidth channel, the wetted perimeter is a constant: P = T = 1. Therefore, a hydraulically wide channel is alternatively defined as that for which the wetted perimeter is a constant. In practice, most natural channels are hydraulically wide (Fig. 217).
Hydraulics of the cross section The dischargeflow area rating in openchannel flow is:
The asymptotic values of β are (Section 1.3):
For trapezoidal channels, values of β lie between the
values for hydraulically wide and triangular channels. Typical values of
β for trapezoidal channels lie approximately
in the range
Depth of flow and depthofflow section There are two related depths of openchannel flow (Fig. 219):
The depth of flow y is the vertical distance from the free surface to the lowest point in the channel cross section. The depthofflow section d is the distance, normal to the direction of flow, measured from the free surface to the lowest point in the channel cross section.
The relation between depth of flow y and depth of flow section d is:
Geometric elements
Table 21 shows geometric elements for four commonly used crosssectional shapes.
Use 2.3 VELOCITY DISTRIBUTION
The mean velocity in openchannel flow is:
Local velocities, however, are likely to vary widely. Vertical velocity profiles vary from zero at the boundary (the noslip condition at the channel bottom) to values slightly greater than the mean near the water surface (Fig. 220).
Transversal velocities are also likely to vary widely, from zero at the side boundaries to maximum values at or near the middle of the channel (Fig. 221). In meandering channels, or channels of curved alignment, velocities are larger along the outside of the bend and smaller on the inside. However, for hydraulically wide channels, the sides have a negligible influence on the flow. In this case, the flow is effectively twodimensional (in the longitudinal and vertical directions).
The assumption of mean velocity V (Eq. 210) further reduces the flow to a statement of onedimensionality (in the longitudinal direction). This assumption is strictly applicable to channels that are relatively straight and for which flows remain inbank. As a convenient approximation, the onedimensional assumption has been applied to channels with mild meandering tendencies and limited overbank flows. However, the onedimensional assumption generally breaks down for channels of large sinuosity and/or substantial overbank flows (Fig. 222).
2.4 MEASUREMENTS OF VELOCITY
Measurements of velocity are commonly performed using a current meter. Current meters measure flow velocity by counting the number of revolutions per second of the meter assembly. The rotation can be around a vertical axis, leading to the cup meter, or around a horizontal axis, leading to the propeller meter. Cup meters are widely used in the United States. The most common type of cup meter is the Price current meter, which has six cups mounted on a vertical axis (Fig. 223). The flow velocity is proportional to the angular velocity of the meter rotor. The flow velocity is determined by counting the number of revolutions per second of the rotor and consulting the meter calibration table.
Discharge measurements. A discharge measurement at a stream cross section requires the determination of flow area and mean velocity for a given stage. The cross section should be perpendicular to the flow, and mean velocity should be based on a sufficient number of velocity measurements across the section. In a typical streamgaging procedure, each of several depth soundings, usually 20 to 30, defines the position of a vertical (Fig. 224). Each depth sounding is associated with a partial section of the stream. A partial section is a rectangle of depth equal to the sounding and of width equal to half the difference of the distances to adjacent verticals. At each vertical, the following observations are made:
In the twopoint method, the current meter is positioned at 0.2 and 0.8 of the flow depth. In the one point method, the current meter is positioned at 0.6 of the flow depth, measured from the water surface. The average of the velocities at 0.2 and 0.8 depth or the single velocity at 0.6 depth is taken as the mean velocity in the vertical. Where a twopoint measurement is impractical (e.g., in very shallow streams), the onepoint method is recommended. For each partial section, the discharge is calculated as:
in which q = discharge, v = mean velocity, and a = flow area. The total stream discharge Q is the sum of the discharges of each partial section. Price current meters types AA and A are used for twopoint velocity measurements in streams with flow depths above 0.75 m and for onepoint measurements in streams with depths ranging from 0.45 to 0.75 m. The dwarf (or pigmy) current meter is used for onepoint measurements in shallow streams or laboratory flumes with depths in the range 0.10 to 0.45 m. Techniques for measuring stream velocity with a current meter vary with stream size. If the stream is wadable, the meter is affixed to a graduated depth rod. If the stream is too deep to wade, the meter is suspended on a cable and is held in the water with a sounding weight. The weights are made of various sizes, from 6.8 kg to 135 kg. Measurements using cable suspension are made from bridges, cableways, or boats (Fig. 225). For the heavier sounding weights or when using a boat, a sounding reel may be required.
2.5 VELOCITY DISTRIBUTION COEFFICIENTS
Due to the nonuniform velocity distribution over a cross section, the true velocity head h_{v} is greater than the velocity head computed based on the mean velocity V. Generally, the true velocity head is:
where in this case α refers to the energy coefficient, or Coriolis coefficient. Values of α range from about 1.03 to 1.36 for fairly straight prismatic channels. The higher values correspond to smaller channels and the lower values to larger channels. Similarly to the case of energy, momentum also requires a correction due to the nonuniform velocities (Fig. 226). The true expression for momentum flux (force) is:
where in this case β refers to the momentum coefficient, or Boussinesq coefficient; and ρ = mass density of water. Values of β range from about 1.01 to 1.12 for fairly straight prismatic channels.
Values of α and β are slightly greater than 1, with α being always greater than β.
For channels of composite cross section, values of α and β can easily get as great as
1.6 and 1.2, respectively
The Coriolis coefficient Assume:
The mean velocity is defined as:
In general, energy is equal to a force integrated over a distance, or force times length:
The kinetic energy for the total area A is equal to mass M times acceleration times distance:
The kinetic energy for the incremental area ΔA is:
The velocity head through ΔA is the kinetic energy divided by the weight, where weight = mg :
The volumetric flux through ΔA is:
The weight flux through ΔA is:
in which γ = unit weight of water.
The incremental kinetic energy flux through ΔA
is equal to the kinetic energy per weight h_{v}
The sum of kinetic energy fluxes for all incremental areas is:
The kinetic energy flux through the total area A, based on mean velocity V, is:
Equating Eqs. 222 and 223, and solving for the Coriolis energy coefficient:
The Boussinesq coefficient
The mass flux
J through the total area A is equal to the mass density ρ times the
volumetric flux
The mass flux through the incremental area ΔA is equal to the mass density ρ times the incremental volumetric flux ΔQ = v ΔA:
In general, momentum M is equal to a force integrated over a period of time, or mass times velocity:
The momentum flux, or force F, is equal to the mass flux times the velocity. Thus, the momentum flux through the incremental area ΔA is:
The sum of all momentum fluxes, or sum of forces for all the incremental areas is:
The momentum flux, or force F, through the total area is:
Equating Eqs. 229 and 230, and solving for the Boussinesq momentum coefficient:
Approximate formulations of α and β While Eqs. 224 and 231 are accurate, they require detailed measurement of the velocity distribution in the cross section of interest. Alternatively, when only the mean velocity V and maximum velocity V_{max} are known, the following formulas may be used to calculate approximate values of the Coriolis and Boussinesq coefficients (Chow, 1959). Defining:
Assuming a logarithmic velocity distribution, the coefficients may be approximated as:
On the other hand, assuming a linear velocity distribution:
2.6 PRESSURE DISTRIBUTION
The pressure distribution along the flow depth in an open channel varies with the shape of the channel bottom relative to the shape of the water surface, measured along the direction of flow. There are three possible cases: (1) parallel flow, (2) convex curvilinear flow, and (3) concave curvilinear flow. Parallel flow Under parallel flow, the channel bottom is relatively straight and it is either: (a) parallel to the water surface, as with uniform flow (Fig. 228), or (b) approximately parallel to the water surface, as with gradually varied flow. In this case, the pressure distribution is essentially hydrostatic, with the pressure varying as a linear function of partial flow depth (line AB in Fig. 228). At the partial flow depth h_{s}, the pressure is: p_{s} = γ h_{s}. In other words, a piezometer located at the partial depth h_{s} below the water surface would rise to the elevation of the water surface.
In practice, uniform flow
and gradually varied flow feature a hydrostatic pressure distribution
Convex curvilinear flow Under convex curvilinear flow,
the channel
bottom is substantially curved,
featuring a convex profile in the vertical plane (Fig. 230).
In this case,
the pressure distribution is nonhydrostatic, with the pressure along the flow depth
varying as a nonlinear function of
partial flow depth (curve AB' in
In practice, rapidly varied flow, e.g., flow over the crest of an ogee spillway, features a nonhydrostatic pressure distribution (Fig. 231). This distribution is characterized by substantial velocity components and accelerations in the direction normal to the flow.
Concave curvilinear flow Under concave curvilinear flow,
the channel
bottom is substantially curved, featuring a concave profile in the vertical plane (Fig. 232).
In this case,
the pressure distribution is nonhydrostatic, with the pressure along the flow depth
varying as a nonlinear function of partial flow depth (curve AB'
in
In practice, rapidly varied flow, e.g., flow at or near the toe of a spillway, features a nonhydrostatic pressure distribution (Fig. 233). This distribution is characterized by substantial velocity components and accelerations in the direction normal to the flow.
The centrifugal pressure head c can be approximately calculated as follows:
The mass per unit of area is:
in which d = flow depth. The centrifugal acceleration is:
in which r = radius of curvature of the streamlines. Thus, the centrifugal pressure is Eq. 237 times Eq. 238:
and the centrifugal pressure head is:
The rise is negative for convex curvilinear flow and positive for concave curvilinear flow (Fig. 234).
Effect of slope on pressure distribution Figure 235 shows a schematic of the pressure distribution in a channel of steep slope θ. Note the following:
For a channel of small slope, h ≅ y, and the vertical depth y may be used to estimate the pressure rise h. However, for a channel of large slope, the difference may be substantial. A 10% slope (i.e., a slope equal to 0.1) corresponds to an angle θ = 5.7°, for which cos^{2} (5.7°) = 0.99. Thus, for a slope greater than 10%, the error in taking the vertical depth y in lieu of the pressure rise h is more than 1%. A channel with slope greater than 10% is referred to as a channel of large slope.
In practice, a channel of large slope features high velocities, which may lead to air entrainment, volume swell, and consequent increase in depth and decrease in density. Thus, the pressure calculated by Eq. 241 may be somewhat higher that the actual value. QUESTIONS
PROBLEMS
REFERENCES
Chow, V. T. 1959. Openchannel Hydraulics. McGraw Hill, New York. Ponce, V. M., and D. Windingland. 1985. Kinematic shock: Sensitivity analysis. Journal of Hydraulic Engineering, ASCE, Vol. 111, No. 4, April, 600611.

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