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<br />EM 1110-2-1601 <br />1 Jul 91 <br /> <br />velocity head may be used. This method under the same <br />circumstances may be applied to bridge openings contain. <br />ing piers. <br /> <br />b. Pier losses. Rapid. tranquil, or a combination of <br />rapid- and tranquil-flow conditions may occur where only <br />bridge piers are located in the flow area. Flow through <br />bridge piers for this condition is classified as class A. B, <br />or C. according to the depth of flow in relation to critical <br />depth occurring upstream, between piers, and downstream. <br />Plate 10 is a graphic description of these classes, which <br />are discussed below. Plate 11 is useful in determining the <br />class of flow in rectangular channels. <br /> <br />(I) Class A flow (energy method). Chow (1959, <br />paragraph 17-10) presents a discussion and several energy <br />loss formulae with appropriate coefficients that may be <br />used for computing bridge pier losses for tranquil flow <br />(class A). While the momentum method presented below <br />may also be used for class A flow, thc energy method <br />usually gives better results. <br /> <br />(2) Classes B and C flows (momentwn method). <br /> <br />(a) A graph (example shown in Plate 12) constructed <br />from the equation proposed by Koch and Carstanjen <br />(Chow 1959) and based on the momentum relation can be <br />used for determining graphically the flow classification at <br />constrictions due to bridge piers. In addition, the graph <br />can be used for estimating unknown flow depths. A <br />summary of the equation derivation follows. <br /> <br />(b) In a given channel section the momentum per <br />unit time of the flow can be expressed by <br /> <br />M = ~ l ~V) <br /> <br />(2.12) <br /> <br />where <br /> <br />M = momentum per unit time, pounds (lb) <br />(from pounds-second per second <br />(lb-sec/sec)) <br /> <br />~ = momentum correction coefficient <br /> <br />'Y = specific weight of water, pounds per <br />cubic foot (pel) <br /> <br />Q = total discharge. cfs <br /> <br />2-6 <br /> <br />v = average channel velocity. feet per <br />second (fps) <br /> <br />e <br /> <br />g = acceleration of gravity, ft/sec2 <br /> <br />In Equation 2-12 ~ is generally assumed to be equal to <br />1.0. Since <br /> <br />Q = AV <br /> <br />(2-13) <br /> <br />Equation 12 can be written <br /> <br />. <br /> <br />2 <br />M = 'YQ <br />gA <br /> <br />(2-14) <br /> <br />(c) The total hydrostatic force m (in pounds) in the <br />channel section can be expressed as <br /> <br />m = riA <br /> <br />(2-15) <br /> <br />where y is the distance from the water surface to the <br />center of gravity (centroid) of the flow section. <br /> <br />e <br /> <br />(d) Combining Equations 14 and 15 results in <br /> <br />2 <br />m+M=riA+J!2- <br />gA <br /> <br />(2-16) <br /> <br />By the momentum principle in an unconstricted channel <br /> <br />. <br /> <br />2 <br />ma ,+ 'YQ <br />gAa <br /> <br />'YQ2 <br />+- <br />gAb <br /> <br />(2-17) <br /> <br />= mb <br /> <br />where ma and mb are the total hydrostatic forces of <br />water in the upstre.am and downstream sections, <br />respectively, lb. <br /> <br />(e) Based on experiments under all conditions of <br />open-channel flow where the channel was constricted by <br />short, flat surraces perpendicular to the flow. such as with <br /> <br />e <br />