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Venturimeter with CO2 and meriam oil

Short answer

p1-p2 = (827-3)×9.81×0.08 = 647 Pa, so p2≈169.35 kPa. Throat velocity V2 = sqrt(2×647/(3×0.8704))≈22.26 m/s, Q=A2 V2≈0.0629 m^3/s (226.5 m^3/h).

In figure below the flowing fluid is CO₂ (density = 3 kg/m³). Neglect losses. If p1p_1 = 170 kPa and the manometer fluid is meriam red oil (S.G = 0.827). Estimate: (a) p2p_2 and (b) the gas rate in m³/h. [Figure: horizontal venturimeter with d1d_1 = 10 cm, d2d_2 = 6 cm and a U-tube manometer reading 8 cm]

Given: CO₂ density ρ=3\rho = 3 kg/m³, p1=170p_1 = 170 kPa, manometer fluid S.G. = 0.827 (ρm=827\rho_m = 827 kg/m³), manometer reading h=8h = 8 cm =0.08= 0.08 m, d1=10d_1 = 10 cm, d2=6d_2 = 6 cm. The gas is treated as incompressible (small pressure change), horizontal meter, no losses.

(a) Pressure at the throat

The U-tube manometer measures the pressure difference between sections 1 and 2:

p1−p2=(ρm−ρ) g h=(827−3)(9.81)(0.08)=646.7 Pap_1 - p_2 = (\rho_m - \rho)\,g\,h = (827 - 3)(9.81)(0.08) = 646.7\ \text{Pa} p2=170 000−646.7=169 353 Pa≈169.35 kPap_2 = 170\,000 - 646.7 = 169\,353\ \text{Pa} \approx 169.35\ \text{kPa}

(b) Gas rate

β=d2d1=0.6,β4=0.1296\beta = \frac{d_2}{d_1} = 0.6,\qquad \beta^4 = 0.1296

Bernoulli with continuity: p1−p2=ρ2V22(1−β4)p_1 - p_2 = \dfrac{\rho}{2}V_2^2\left(1 - \beta^4\right).

V2=2(646.7)3×0.8704=495.3=22.26 m/sV_2 = \sqrt{\frac{2(646.7)}{3\times 0.8704}} = \sqrt{495.3} = 22.26\ \text{m/s} A2=π4(0.06)2=2.827×10−3 m2Q=A2V2=0.06293 m3/s=226.5 m3/h\begin{aligned} A_2 &= \frac{\pi}{4}(0.06)^2 = 2.827\times 10^{-3}\ \text{m}^2\\ Q &= A_2V_2 = 0.06293\ \text{m}^3/\text{s} = 226.5\ \text{m}^3/\text{h} \end{aligned}

Answer: (a) p2≈169.35p_2 \approx 169.35 kPa; (b) Q≈0.0629Q \approx 0.0629 m³/s ≈226.5\approx 226.5 m³/h.

✓ Answer checked by Claude Opus 5.5 (high effort)

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