Question #37032

A liquid of density 1.17 × 103 kg/m3 flows steadily through a pipe of varying diameter and height. At location 1 along the pipe the flow speed is 9.47 m/s and the pipe diameter is 1.11 × 101 cm. At location 2 the pipe diameter is 1.77 × 101 cm. At location 1 the pipe is 9.45 m higher than it is at location 2. Ignoring viscosity, calculate the difference between the fluid pressure at location 2 and the fluid pressure at location 1.

Expert's answer

A liquid of density 1.17×103kg/m31.17 \times 103 \, \mathrm{kg/m^3} flows steadily through a pipe of varying diameter and height. At location 1 along the pipe the flow speed is 9.47m/s9.47 \, \mathrm{m/s} and the pipe diameter is 1.11×101cm1.11 \times 101 \, \mathrm{cm}. At location 2 the pipe diameter is 1.77×101cm1.77 \times 101 \, \mathrm{cm}. At location 1 the pipe is 9.45m9.45 \, \mathrm{m} higher than it is at location 2. Ignoring viscosity, calculate the difference between the fluid pressure at location 2 and the fluid pressure at location 1.

Solution

From the equation of continuity:


A1v1=A2v2,A_1 v_1 = A_2 v_2,


where A1=πd124A_1 = \frac{\pi d_1^2}{4}, A2=πd224A_2 = \frac{\pi d_2^2}{4} — areas of pipes.

So


v2=A1A2v1=πd124πd224v1=d12d22v1.v_2 = \frac{A_1}{A_2} v_1 = \frac{\frac{\pi d_1^2}{4}}{\frac{\pi d_2^2}{4}} v_1 = \frac{d_1^2}{d_2^2} v_1.


Use Bernoulli's equation


P2+ρgz2+ρv222=P1+ρgz1+ρv122.P_2 + \rho g z_2 + \frac{\rho v_2^2}{2} = P_1 + \rho g z_1 + \frac{\rho v_1^2}{2}.


The difference between the fluid pressure at location 2 and the fluid pressure at location 1:


P2P1=ρg(z1z2)+ρ(v12v22)2=ρg(z1z2)+12ρv12(1(d1d2)4).P_2 - P_1 = \rho g (z_1 - z_2) + \frac{\rho (v_1^2 - v_2^2)}{2} = \rho g (z_1 - z_2) + \frac{1}{2} \rho v_1^2 \left(1 - \left(\frac{d_1}{d_2}\right)^4\right).P2P1=1.171039.819.45+121.171039.472(1(1.111.77)4).P_2 - P_1 = 1.17 * 10^3 * 9.81 * 9.45 + \frac{1}{2} * 1.17 * 10^3 * 9.47^2 \left(1 - \left(\frac{1.11}{1.77}\right)^4\right).P2P1=1.53105Pa=153kPa.P_2 - P_1 = 1.53 * 10^5 P a = 153 \, kPa.


Answer: 153kPa153 \, kPa.

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