|
<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 />
|