The equation for flow distribution and head losses are written.
The friction factor is computed for given flow rate assuming smooth
wall using Prandtl relation for turbulent flows. The equations for
flow rate and head losses are simultaneous equations which are
solved iteratively bu assuming the intial solution and updating
till the convergence is achieved. The solution of simultaneous
equation gives us the Za, v2, v3, v4, v5. Once we know the
velocity, we can find the flow rate to the respective tanks. Note:
There is a typo in the problem. The datum given should be zB = 101,
zC = 55 and zD =30 but in the first line zA, zB and zC are
given.
LO 200 14/ 11 -0.2 . 2x9.81 (307 100] 200 Q = 8 + 8 5 (30) ² U = 15 (26) ² 0 + 1 (20) a 9v, Ilvtvg 4 - ① G = Q & Q 21 (20) og = 1 (20) ² + 2 (20) ² » Ug = y + - • 2 F 24-105(0.002), )* ***60**) - **5); ADA ***E SCO ALEXA 2-3 0-009 «{) Q = 1 = 1 1 10.3)” U = 0,5 14,15 ml S - -x14. O 0.009 2x9.81 0.3 0.009 2x9.81 F = 2 by (he f') -0.8 f = 0.009 (Smouth wall Pipe Re - pu, d, 1000) * 14.15* 0. 3 4708687.433 (Turbodent) (8.9x104)
gv = 40 + 40 - 127-35/4 = V2 + V V₂ + ₂ = 31.8 - 6 y = y + vs - . za - 101 = 61:23 +(0.09) 2-3 34-55 = 61-23 + (0-1376) y2 + (0.946), -6 ZA - 30 = 61.23 + (0-1370) vx2 +(0:09) - © Equating 4 & €1-23 +55 + (0-1376) x (0+)+(0.1146) 4,2 - 61-23 +36 +601376) (4 * vs)+(0109) v" 25+ (0.1146) v = 0.09 v ². per 101461.23 + 0.09% (31-8 –(+v)]* =*p55+61-23 + 04346 (,+v)*+ (0-11416)? 46 +2.862 7 0.09 ( +v) = 0.134C (4,+V_)* +(0140) y, 48-862 = (0-2276) (+V_)*+601146),? Solving the above sen sinut écouleurly iteratively will give Q=Bdku x 02 x 12 = 0.376 mils u = 5.84 m/s exy = lex - x 5.84 = 0.1835 mils V = 14:15 mlo ZA = 175.2m " x 0.2 x 14.15 = 0.445 m3/s. 2 x м o.. = 12 Rater Flow X 0.2 V = 12 m/s V = 20ls C Dų