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� � <br /> Rectangular Channel Analysie & Desiqn <br /> Opon Char..nel - Uniform flow <br /> warksheet Name: Boeing 4L-41 <br /> Comme�t: Patigue test ela.b aontainivant <br /> Solve For Depth <br /> civon input Data: <br /> Bottom Width. . . . . 1. 5o ft <br /> Manning�s n. . . . . . 0.025 <br /> Channel 91ope. . . , 0.0016 Pt/ft <br /> D180hHrge. . . . . . . . �13 efs � <br /> Computed Results: <br /> Depth. . . . . . . . . . . 1.04 ft <br /> Velocity. . . . . . . . . 1.37 fps <br /> Flow Area. . . . 1.55 sf <br /> FloW Top Wiflth. . . 1. 50 ft <br /> Wstted Perimatex. 3.88 ft <br /> Critical Depth. . . 0.4o Pt <br /> Critical Sloye. . . o.o2ie it/ft <br /> Frouda Number. . . . 0.24 (flow is Subcritical) <br /> FArT�Gru E TFs&"f" S�Jk'3 "l7z�--�t� <br /> Open Channel Flow Modu:.e, Var�ion 3.41 (c) 1991 <br /> Haestad Methods, inc. +� 37 Srookside Rd * Waterbury, Ct 06708 <br />� <br />, . <br /> [laoJ «< lao.36 a» 10/21j92 - 16:28 Page 3 <br />