Ans) We know,
Q = A x V
=> u1 = (Q / A1) Cos (30)
= (0.11 / 0.0081) Cos(30)
= - 11.77 m/s ( Negative sign due to flow direction)
=> v1 = (Q / A1) Sin (30)
= (0.11 / 0.0081) Sin(30)
= 6.8 m/s
= -11.77 i + 6.8 j
Now,
=> u2 = Q / A2
= 0.11 / 0.0182
= - 6.04 m/s
=> v2 = Q/A2
Since, here in no inclination v2 = 0
= - 6.04 i
Now, sum of horizontal force = 0
=> - V2 Cos(30) u2 P A2 + V1 P1 u1 A1 + Rx = P2A2 Cos(30) - P1 A1
=> Rx = P2A2 Cos(30) - P1 A1 + V2 Cos(30) u2 P A2 - V1 P1 u1 A1
=> Rx = P2 (0.0182)(0.866) - 15000(0.0081) + 9724.37
=> Rx = 0.0158 P2 - 9602.9
Sum of vertical forces = 0
=> Ry = P1A1Sin(30) + Ww + Welbow - v1 P1 A1 u1 + v1 Sin(30)P A2 v2
=> Ry = 15000(0.0081)(0.5) + 0 + (10 x 9.81) + 9724.4
=> Ry = 9.83 kN
To determine Gauge pressure P1 apply Bernoulli equation,
P1 / g + V12/2g + Z1 = P2 /g + V22/2g + Z2
Since elevation is same, Z1 =Z2 =0
=> P2 / = P1/g + V12 / 2 - V22/ 2
V1 = 0.11 / 0.0081 = 13.6 m/s
V2 = 6.04 m/s
=> P2 = [(15 / 9.81) + 13.62 / 2 - 6.042/2 ]
= (1.53 + 92.48 - 18.06) kPa
= 75.94 kPa
Hence, Rx = 0.0158(75940) - 9602.9
= - 8.4 kN
Ry = 9.83 kN
P2 =75.94 kPa
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