Laserfiche WebLink
<br />Chapter II.-COMPUTATION OF BACKWATER <br /> <br />2.1 Expression for backwater, Bridge back- <br />water analysis is far from simple regardless of the <br />method employed, Many minor as well as major <br />variables are involved in any single waterway <br />problem, For the model which was installed in a <br />rectangular flume and operated with uniform rough- <br />ness, minor variables such as type and geometry of <br />abutments, width of abutments, slope of embank- <br />ments, roadway widths and width to depth ratio <br />could be evaluated in relation to the Froude Number <br />as was done in the comprehensive model study report <br />(18). In the case of bridges in the field where rough- <br />ness of flood plain and main channel differ materially <br />and channel cross sections are irregular, the Froude <br />Number is no longer a meaningful parameter and <br />minor variables lose their significance. This is es- <br />pecially true as bridge length is increased. Fortu- <br />nately, reasonable accuracy is acceptable in most <br />bridge backwater solutions, thus, a practical method, <br />utilizing the dominant variables, is presented in thi8 <br />chapter for computing backwater produced by <br />bridge constrictions. <br />A practical expression for backwater has been <br />formulated by applying the principle of conserva- <br />tion of energy between the point of maximum back- <br />water upstream from the bridge, section I, and a <br />point downstream from the bridge at which normal <br />stage has been reestablished, section 4 (fig, 2A), The <br />expression is reasonably valid if the channel in the <br />vicinity of the bridge i8 essentially straight, the <br />cross sectional area of the stream is fairly uniform, <br />the gradient of the bottom is approximately con- <br />stant between sections 1 and 4, the flow is free to <br />contract and expand, there is no appreciable scour <br />of the bed in the constriction and the flow is in the <br />subcritical range. <br />The expression for computation of backwater up- <br />stream from a bridge constricting the flow, which is <br />developed in the comprehensive report (18), is as <br />follows: <br /> <br />h,' = K'", ~'; + '" [(~:')' - e7)'] ~~' (4) <br /> <br />Where <br /> <br />h,' = total backwater (ft.). <br />K' ~ total backwater coefficient. <br />'" & '" = as defined in expressions 3a and 3b (sec, <br />1.11). <br />An2 = gross water area in constriction measured <br />below normal stage (sq, ft,), <br />Vn, = average velocity in constriction' or Q/ An' <br />(f,p,s,), <br />A, = water area at section 4 where normal stage <br />is reestablished (sq, ft.), <br />A, = total water area at section 1, including <br />that produced by the backwater (sq. ft,), <br /> <br />To compute backwater, it is necessary to obtain <br />the approximate value of h,' by using the first part <br />of expression (4) : <br /> <br />V2n2 <br />h1* = K*ot.2- <br />2g <br /> <br />(4a) <br /> <br />The value of A dn the second part of expression (4), <br />which depends on h,', can then be determined and <br />the second term of the expression evaluated: <br /> <br />'" [e:')' - e:')'] v;;' (4b) <br /> <br />This part of the expression represents the difference <br />in kinetic energy between sections 4 and 1, expressed <br />in terms of the velocity head, V'n2/2g, Expression <br />(4) may appear cumbersome, but this is not the case, <br />Since the comprehensive report (18) is generally <br />not available, a concise explanation regarding the <br />development of the above backwater expression and <br />the losses involved is included in appendix A of this <br />bulletin under type I flow, <br />2.2 Baekwater coefficient. Two symbols are <br />interchangeably used throughout the text and both <br />are backwater coefficients. The symbol K. is the <br />backwater coefficient for a bridge in which only the <br />bridge opening ratio, M, is considered, This is known <br /> <br />* The velocity, Vn,l. is not an actual mea6urable velocity, but represents a <br />reference velocity readily computed for both model and field structurelI. <br /> <br />13 <br />