Laserfiche WebLink
<br />EM 1110-2.1416 <br />15 Oct 93 <br /> <br />@ ~ <br />i--=-- -=- - -=- - ~ EnergY-Grade Line - - ~ he <br /> <br />2 <br />(X2V2 <br />2g <br /> <br />~ Water Surface <br /> <br />2 <br />(X,V, <br />2g <br /> <br />Flow <br /> <br />~ <br /> <br />WS2 <br /> <br />WS, <br /> <br /> <br />Figure 6-1. Open chennel energy re18tionehips <br /> <br />~y2 !XIy2 <br />WS+ 2=w.o+ I h <br />2"""2g""" " I """2g""" + e <br /> <br />(6-2) <br /> <br />An equation for the energy head loss he can be written as <br />follows <br /> <br />2 2 <br />- ~Y2 !XIYI <br />he = LSf + CI_ - -I <br />2g 2g <br /> <br />(6-3) <br /> <br />where <br /> <br />L = discharge weighted reach length <br />~ = representative friction slope for reach <br />C = expansion or con1raction loss coefficient <br /> <br />The solution of Equation 6-2 is the basis of water surface <br />profile computations in programs such as HEC-2. The <br />standard step method used to obtain a solution requires <br />successive approximations. A trial value of WS2 in <br />Equation 6-2 is assumed, and values for he and change in <br />velocity head are computed and summed to obtain ~WS. <br />This value is added to the known downstream water <br />surface elevation 10 compute WS2. The difference <br />between trial and computed values converges with suc- <br />cessive trials. The steps in this procedure are as follows: <br /> <br />6-2 <br /> <br />a. Assume a water surface elevation at the upstream <br />cross section (or downstream cross section if a supercriti- <br />cal proftle is being calculated). <br /> <br />b. Based on the assumed water surface elevation, <br />determine the corresponding Iotal conveyance and veloc- <br />ity head. <br /> <br />c. With values from step 2, compute ~ and solve <br />Equation 6-2 for he' <br /> <br />d. With values from steps 2 and 3, solve Equa- <br />tion 6-2 for WS2. <br /> <br />e. Compare the computed value of WS2 with the <br />values assumed in step I; repeat steps I through 5 until <br />the values agree to within .01 feet (or .01 meters). <br /> <br />6-4. Range of Applicability <br /> <br />The assumptions of the method as described in sec- <br />tion 6-2 are the basis for determining applicability. Their <br />effects in modeling are as follows: <br /> <br />e <br /> <br />'I <br /> <br />. <br /> <br />1. <br /> <br />. <br /> <br />~ <br /> <br />.1;, <br /> <br />e <br />