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<br /> <br />,- <br /> <br />Andrews and Nelson <br /> <br />469 <br /> <br />Finally, the interrelation of these three elements and their combination into a <br />topographic evolution model is briefly discussed. <br /> <br />The Flow Model <br /> <br />The fundamental requirement of a coupled flow-bed topography model is a <br />careful treatment of the fluid dynamics. In particular, the response of the flow to <br />topographic non uniformity must be treated accurately, because the forcing on the <br />flow field due to the nonuniformity of the bed has a significant influence upon the <br />topography. It has been demonstrated [Yen and Yen, 1971; Dietrich and Smith, <br />1983; Berg and Odgaard, 1988] that the convective accelerations due to planform <br />and topographic nonuniformity in channels are often of the same order of magnitude <br />as the pressure gradient and stress divergence in the local momentum balance. <br />Thus, a model that is based upon a perturbation expansion a.bout a. zero-order <br />steady uniform flow will not provide a satisfactory simulation of conditions in a <br />reach with complex topography. Accordingly, the non-linear treatment originally <br />developed by Smith and McLean [1984] and subsequently expanded upon and <br />applied to the mobile bed by Nelson and Smith [1989a., b, this volume] is employed <br />here. The mathematical development of this treatment is presented in detail in the <br />above work, and will not be repeated here. In order to interpret the results of the <br />evolution model presented below, however, it is useful to briefly restate the basic <br />assumptions used in developing the flow model. They are as follows: <br /> <br />The flow is treated as quasi-ilteady. <br />The pressure distribution is assumed to be hydrostatic. <br />Lateral stresses and boundary layers are neglected. <br />The vertical velocity and length scales are an order of magnitude smaller <br />than the crosS-iltream velocity and length scales which are, in turn, an order <br />of magnitude smaller than the streamwise velocity and length scales. <br />The vertical structure of the zero-order streamwise velocity field is given by <br />a similarity structure (e.g., a logarithmic or quasi-logarithmic profile). One <br />of the consequences of this assumption is that, at lowest order, the <br />boundary shear stress is related to the vertically-averaged velocity field by <br />a drag coefficient (Note that this coefficient depends upon local roughness <br />and is not necessarily spatially constant). <br />Cross-iltream secondary flows associated with both channel planform and <br />streamline curvature are evaluated. <br />Advection of streamwise and crOSS-iltream momentum fluxes by the <br />secondary flows are neglected [although they may be included iteratively, <br />see Nelson and Smith, 1988b]. <br /> <br />The inputs required for this computational model are the planform and <br />topography of the channel, the local roughness lengths in the channel, and the <br />discharge. The flow model computes three-dimensional velocity fields; downstream <br />and cl'OSS-6tream boundary shear stresses, and water-ilurface elevation in the <br />channel. The predicted values can be expected to reproduce the actual values with <br />reasonable accuracy, provided that none of the assumptions above are violated. In <br />practice, the assumptions restrict the application of this model to channels where <br />depths are substantially smaller than widths and streamwise variations in width and <br />topography are gentle. Thus, the model is not valid for the case of rapid width <br />variations (i.e., banks at angles greater than twenty or thirty degrees to the <br />downchannel direction), and cannot be expected to give good results if largEHlcale <br />bed slopes along the direction of fluid motion exceed ten d~ees or so. These <br />situations, however, are relatively uncommon, especially in allUVial channels. <br /> <br />.1. <br />"2. <br />3. <br />4. <br /> <br />5. <br /> <br />6. <br /> <br />7. <br /> <br />.';-.' -', "', <br /> <br /> <br /> <br />