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<br />EM 1110-2.1601 <br />1 Jul 91 <br /> <br />4-5 Hydraulic Model Studies <br /> <br />a. General. The use of hydraulic models has <br />become a standard procedure in the design of cQmplex <br />open channels not subject to analytical analyses or for <br />which existing design criteria based on available model <br />and field tests are inadequate. Hydraulic models afford a <br />means of checking peIformance and devising modifICa- <br />tions to obtain the best possible design at minimum cost. <br />Model tests should be used to supplement but not replace <br />theoretical knowledge, good judgment. and experience of <br />the design engineer. They often indicate design changes <br />that save substantial amounts in consa-uction costs as well <br />as effect improvements in operation. Model tests of large <br />flood conlrOl channels are generally desirable where sup- <br />ercritical flow results in standing waves and other major <br />disturbances in channels containing junctions, transition <br />SlrUClUreS, alignment curvature, multiple bridge piers, or <br />stilling basins. <br /> <br />b. Model design. <br /> <br />(I) The theory of model design is lre:lted in <br />EM 1110-2-1602 and other publications (Rouse 1950, <br />Davis and Sorenson (1969), American Sociery of Civil <br />Engineers (ASCE) 1942). For open channel models, the <br />gravity force will dominate the now and similitude will <br />require equality of Froude number in the model and pro- <br />totype. The Froudian scale relations (model-to-prototype) <br />in Table 4-1 apply to undistorted models. The length ratio <br />Lr is the model-to- prototype ratio Ln/Lp. These <br />lransfer relations are based on equal force of gravity and <br />density of fluid in model and prototype. The procedure <br />for initiation of model studies is discussed in <br />EM 1110-2.1602. <br /> <br />(2) Model scale ratios for nood conlrOl channels <br />have ranged from 1:15 to 1:70. depending on the type of <br />problem being studied. the relative roughness of the <br />model and prototype, and the size of the prototype SlrOC- <br />ture. Scale ratios of 1:15 to 1:30 are usually employed <br /> <br />where supercritical flow wave problems are involved. <br />They are also used for sectional models of drop SlrUC- <br />lUreS, spillways, etc. The smailer scale ratios (1:30 to <br />1:70) are used for general model studies where long chan- <br />nel lengths are reproduced. The accuracy of possible <br />model consa-uction and flow measurements may conlrOl <br />the permissible scale rntios. Most models of channels are <br />generally built to give depths of flow about 0..5 ft or more <br />and channel widths of about I to 2 ft. The most common <br />scale ratios ased by the USAED, Los Angeles. Hydraulic <br />Labol3lOry for channel model studies are from 1:25 to <br />1:40. <br /> <br />c. Model roughness. Turbulent flow will prevail <br />with model channel velocities and depths commonly used <br />in testing. In most cases, the channel now is <br />rough-turbulent or nearly so: therefore, hydraulic resis- <br />tance is determined primarily by the relative size of the <br />roughness elements. However, the model Reynolds num- <br />ber will always be smaller than the prototype. and this <br />will to some extent c:luse scale distortion of certain phe- <br />nomena such as zones of separation. wave dissipation. <br />flow instability, and turbulence in the model. Particular <br />care should be taken in interpreting those effects that are <br />known to be slrOngly dependent on viscous forces. <br /> <br />d. Slope distorrion. An empirical equation of the <br />Manning type may be used to give the required model <br />roughness (Rouse 1950) for large-scale models where <br />fully rough-turbulent flow prevails. This condition is <br />expressed by the equation <br /> <br />n = L 1/6 <br />r r <br /> <br />(4-9) <br /> <br />If this roughness criterion cannot be fulfilled. slope ad- <br />justment or distortion must be applied to the model so <br />that prototype flow conditions can be simulated in the <br />model The amount of additional slope required is given <br />by the equation (Rouse 1950) <br /> <br />Table 4-1 <br />Scale R.lelione <br /> MannIng'S <br />Langm Area Volume Tune Velocity Discharge n <br />L L2 L3 L1/2 L1/2 L5/2 Ll15 <br />r. r r r r r r <br /> <br />4-8 <br />