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Venturi meter discharge and numerical

Short answer

Discharge Q = Cd a1 a2 / sqrt(a1² - a2²) sqrt(2gh), with h = x(Sm/Sf - 1). Using a1=0.0707 m², a2=0.0177 m², h=2.52 m, Cd=0.98 gives Q = 0.126 m³/s.

(a) Derive the expression for discharge through a horizontal Venturi meter. Differentiate between a Venturi meter and an orifice meter. (b) A Venturi meter has an inlet diameter of 300 mm and a throat diameter of 150 mm. It is connected to a differential U-tube mercury manometer (specific gravity 13.6) which reads 20 cm. The pipe carries water and the coefficient of discharge is 0.98. Find the discharge.

(a) Venturi meter

A Venturi meter consists of a converging cone, a short throat and a diverging cone. The pressure drop between inlet (section 1) and throat (section 2) is used to find the discharge.

   1                2                
   |   converging   |  throat   diverging
 ==\__              _____              __/==
        \__________/     \____________/
   p1 ---|          |--- p2

Apply Bernoulli's equation between 1 and 2 (horizontal, ideal fluid):

p1ρg+V122g=p2ρg+V222g\frac{p_1}{\rho g} + \frac{V_1^2}{2g} = \frac{p_2}{\rho g} + \frac{V_2^2}{2g}

Let h=p1−p2ρgh = \dfrac{p_1 - p_2}{\rho g} (differential head). Continuity: a1V1=a2V2a_1V_1 = a_2V_2, so V1=V2 a2/a1V_1 = V_2\,a_2/a_1.

h=V222g[1−(a2a1)2]⇒V2=a1a12−a222ghh = \frac{V_2^2}{2g}\left[1 - \left(\frac{a_2}{a_1}\right)^2\right] \quad \Rightarrow \quad V_2 = \frac{a_1}{\sqrt{a_1^2 - a_2^2}}\sqrt{2gh}

Theoretical discharge Qth=a2V2Q_{th} = a_2V_2. Including the coefficient of discharge CdC_d (about 0.96 to 0.99) for losses:

Q=Cd a1a2a12−a222ghQ = C_d\,\frac{a_1a_2}{\sqrt{a_1^2 - a_2^2}}\sqrt{2gh}

For a differential mercury manometer with reading xx: h=x(SmSf−1)h = x\left(\dfrac{S_m}{S_f} - 1\right).

BasisVenturi meterOrifice meter
ConstructionCone, throat, diffuserThin plate with sharp hole
Head lossSmall (pressure mostly recovered)Large (no recovery)
CdC_dHigh (0.96 to 0.99)Low (about 0.6 to 0.65)
Cost and sizeCostly, longCheap, compact
UseLarge flows, where energy loss mattersSmall pipes, low cost

(b) Numerical

a1=π4(0.3)2=0.07069 m2,a2=π4(0.15)2=0.01767 m2h=x(13.61−1)=0.2×12.6=2.52 m of water\begin{aligned} a_1 &= \frac{\pi}{4}(0.3)^2 = 0.07069\ \text{m}^2, \quad a_2 = \frac{\pi}{4}(0.15)^2 = 0.01767\ \text{m}^2 \\ h &= x\left(\frac{13.6}{1} - 1\right) = 0.2 \times 12.6 = 2.52\ \text{m of water} \end{aligned} Q=0.98×0.07069×0.017670.070692−0.017672×2×9.81×2.52=0.98×1.2492×10−30.06844×7.032=0.1258 m3/s\begin{aligned} Q &= 0.98 \times \frac{0.07069 \times 0.01767}{\sqrt{0.07069^2 - 0.01767^2}} \times \sqrt{2 \times 9.81 \times 2.52} \\ &= 0.98 \times \frac{1.2492\times10^{-3}}{0.06844} \times 7.032 \\ &= 0.1258\ \text{m}^3/\text{s} \end{aligned}

Velocity at the inlet = 0.1258/0.07069=1.78 m/s0.1258/0.07069 = 1.78\ \text{m/s}, and at the throat = 7.12 m/s7.12\ \text{m/s}.

Answer: Q=0.126 m3/s=126 L/sQ = 0.126\ \text{m}^3/\text{s} = 126\ \text{L/s}

✓ Answer checked by Claude Opus 5.5 (high effort)

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