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04-BS-7 · December 2015

Question 6 of 13: Ideal-Flow Velocity and Flow Rate Through a Sharp-Edged Nozzle

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

04-BS-7 Mechanics of Fluids — December 2015 (National Examinations, three hours, closed book). Section A (Calculative) offers 9 questions and instructs "do seven"; Section B (Analytical) offers 4 questions and instructs "do three." Every question is answered below (13 of 13), so students can use the full paper as a study resource. Constants used throughout (from the paper's own Constants page): g = 9.81 m/s², ρwater = 1000 kg/m³, ρair = 1.19 kg/m³ (20°C) / 1.21 kg/m³ (15°C), μair = 1.8×10⁻⁵ N·s/m², Rair = 287 J/kg·K, Rhelium = 2077 J/kg·K, patm = 100 kPa.

Reference texts: F. M. White, Fluid Mechanics, 8th ed. (McGraw-Hill) — fluid statics and manometry (Ch. 2), control-volume momentum/energy and propulsion (Ch. 3), potential/inviscid flow around cylinders (Ch. 8), viscosity and Newtonian shear (Ch. 1), pipe friction and the Moody chart (Ch. 6), and drag on immersed bodies (Ch. 7).

Question 6: Ideal-Flow Velocity and Flow Rate Through a Sharp-Edged Nozzle (5 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given.

QuantityValue
Pipe diameter D₁40 mm
Jet diameter D₂10 mm
Pipe gauge pressure p₁3 MPa
Jet exit pressure (to atmosphere)0 gauge

Find. V₁ (pipe), V₂ (jet), and Q.

V₁, D₁=40 mmV₂, D₂=10 mmp₁ = 3 MPa (gauge)
Fig. Q6 — ideal (frictionless) acceleration from the 40 mm pipe through the sharp-edged orifice plate into the 10 mm free jet at atmospheric pressure.

Approach. Combine continuity (A₁V₁=A₂V₂) with Bernoulli between the pipe and the jet (no elevation change, ideal flow) to eliminate V₁ and solve directly for V₂.

  1. Continuity relates the two velocities. $$V_1 = \left(\frac{D_2}{D_1}\right)^2 V_2 = \left(\frac{10}{40}\right)^2 V_2 = 0.0625\,V_2$$
  2. Bernoulli between the pipe and the jet (p₂=0 gauge): $$p_1 = \tfrac{1}{2}\rho\left(V_2^2 - V_1^2\right) = \tfrac{1}{2}\rho V_2^2\left(1-0.0625^2\right)$$
  3. Solve for the jet velocity. $$V_2 = \sqrt{\frac{2p_1}{\rho(1-0.0625^2)}} = \sqrt{\frac{2(3\times10^6)}{1000(0.99609)}} = \boxed{77.61\ \text{m/s}}$$
  4. Back out the pipe velocity and the flow rate. $$V_1 = 0.0625(77.61) = \boxed{4.85\ \text{m/s}}$$ $$Q = \frac{\pi}{4}D_2^2\,V_2 = \frac{\pi}{4}(0.010)^2(77.61) = \boxed{6.10\times10^{-3}\ \text{m}^3/\text{s} = 6.10\ \text{L/s}}$$
QuantityResult
Pipe velocity V₁4.85 m/s
Jet velocity V₂77.61 m/s
Flow rate Q6.10 L/s