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Last modified
1/25/2010 6:27:01 PM
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Title
Engineering and Design Hydraulic Design of Flood Control Channels
Date
7/1/1991
Prepared By
US Army Corps of Engineers
Floodplain - Doc Type
Educational/Technical/Reference Information
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<br />(a) Prismatic channels. A prismatic channel is ch3r- <br />acterized by unvarying cross section. constant bottom <br />slope, and relatively straight a1i gnmenl. There are three <br />general methods of derennining flow proftles in this type <br />of channel: direct integrnlion. direct step. and standard <br />step, as discussed in Chow (1959, pp 252-268). The <br />direct integration and direct step methods apply exclu- <br />sively to prismatic channels, whereas the standard step <br />method applies not only to prismatic channels but is the <br />only method to be applied to nonprismatic channels. The <br />direct integrnlion method (with certain restrictions as to <br />the consWlCY of hydraulic exponents) solves the varied <br />flow equation to detennine the length of re:lCh between <br />successive depths. Use is made of varied-flow-function <br />tables to reduce the amount of computations. This <br />method is not nonnally employed unless sufficient <br />profiles and length of channel are involved to warr.mt the <br />amount of precomput:ltional preparation. The direct step <br />method detennines the length of reach between successive <br />depths by solution of the energy and friction equations <br />written for end sections of the reach. The stand:1rd step <br />method is discussed in (b) below. <br /> <br />(b) Nonprismatic channels. When the cross section, <br />alignment. and/or bottom slope changes along the channel, <br />the standard step method (Chow 1959. P 265) is applied. <br />This method detennines the water-surface elevation <br />(depth) at the reach extremity by successive approxima- <br />tions. Trial water-surfuce elevations are assumed until an <br />elevation is found that satisfies the energy and friction <br />equations written for the end sections of the reach. Cross <br />sections for this method should. in general, be selected so <br />that velocities are increasing or decreasing continuously <br />throughout the reach, EM 1110-2-1409 contains further <br />infonnation on this method. Pl3le 8 shows a sample <br />computation for a gradually contracting trapezoidal chan- <br />nel where bOth bottom width and side slope vary. Suc- <br />cessive approximations of water,surface elevations are <br />made until a balance of energy is obtained. Friction <br />losses hr are based on the Manning equation. <br /> <br />Sf ~ <br /> <br />n2V2 <br />2.21R,10 <br /> <br />~ <br /> <br />v2 <br />C"R <br /> <br />(2-1 and 2-2 bis) <br /> <br />For the sample computation a mild slope upstream and <br />Sleep slope downstream of sta 682+40 have been <br />assumed. Critical depth would occur in the vicinity of <br />sta 682+40 and has been assumed as the starting condi- <br />tion. Initially, column 21 has the same value as column <br />10. The computations proceed downstre:lll\ as the flow is <br />rapid. The length of re:JCh is chosen such that the change <br />in velocity between the ends of the reach is less than <br /> <br />EM 111()"2-1SJ1 <br />1 Jul 31 <br /> <br />10 percenl. The energy equation is balanced when <br />column 21 checks column 10 for the trial water surt:JCe of <br />column 5. PI3le 9 repeats the computation, substituting k <br />= 0.002 ft for n = 0.014. For rough channel conditions <br /> <br />C = 32.6 log10 (12/R) <br /> <br />(2-6 bis) <br /> <br />2.3. Flow Through Bridges <br /> <br />Bridge piers 10000ted in channels result in energy losses in <br />the flow and create disturbances at the bridge section and <br />in the channel sections immediately upstre:un and down- <br />stream. As bridge pier losses materially affect W3ler. <br />surface elevations in the vicinity of the bridge, their <br />careful determination is important Submergence of <br />bridge members is not desirable. <br /> <br />a. AbUtment losses. Bridge abutments should not <br />extend into the flow = in rapid, flow channels. In <br />tranquil-flow channels they should be so designed that the <br />flow depth between abutments or between the abutment <br />and an intennedi3le pier is greater than critical depth. <br />The Bureau of Public Roads (BPR) (Bradley 1978) has <br />published design charts for computing backwarer for <br />various abutment geometries and degrees of conlraCtion. <br />The design procedure and charts developed by BPR are <br />recommended for use in channel designs involving bridge <br />abuunents. For preliminary designs. a step b:JCkwaler <br />computation using abrupt expansion and conlraCtion head <br />losses of 1.0 and 0.5. respectively, times the change in <br />velocity head may be used. This method under the s:une <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 cbsses, which <br />are discussed below. Plate 11 is useful in determining the <br />class of flow in rectangular channels. <br /> <br />(1) Class A flow (energy method). Chow (1959. <br />paragraph 17,10) presents a discussion and several energy <br />Joss fonnulae with appropriate coefficients lhm may be <br />used for computing bridge pier losses for tranquil flow <br />(class A). While the momentum method presented below <br /> <br />2-5 <br />
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