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04-BS-7 · December 2015

Question 3 of 13: Stagnation and Side Pressure on a Cylindrical Chimney

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 3: Stagnation and Side Pressure on a Cylindrical Chimney (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
Chimney diameter20 m (height 275 m is not needed — flow is 2-D around the section)
Free-stream wind velocity V₀100 km/h = 27.78 m/s
Air density ρ (20°C)1.19 kg/m³
Surface velocity lawV(θ) = 2V₀sinθ

Find. Velocity and gauge pressure at θ = 0° (point 1, stagnation) and θ = 90° (point 2, side).

CYLINDERV₀ = 27.78 m/s12θPoint 1: V=0, p=+459 PaPoint 2: V=55.56 m/s, p=−1377 Pa
Fig. Q3 — ideal (inviscid) flow around a long cylinder: point 1 is the front stagnation point (θ=0°), point 2 is the side point (θ=90°) where the surface velocity peaks at 2V₀.

Approach. Apply Bernoulli's equation between the undisturbed free stream and each surface point (inviscid, no elevation change), using the given surface-velocity law to fix V at each point.

  1. Velocities from the surface-velocity law. At the stagnation point (θ=0°) and the side point (θ=90°): $$V_1 = 2V_0\sin(0^\circ) = 0, \qquad V_2 = 2V_0\sin(90^\circ) = 2V_0 = 2(27.78) = \boxed{55.56\ \text{m/s}}$$
  2. Bernoulli between free stream and the surface (gauge, no elevation change). $$p(\theta) - p_\infty = \tfrac{1}{2}\rho\left(V_0^2 - V(\theta)^2\right)$$
  3. Gauge pressure at the stagnation point (V=0): $$p_1 = \tfrac{1}{2}(1.19)(27.78^2 - 0) = \boxed{459\ \text{Pa} = 0.459\ \text{kPa}}$$
  4. Gauge pressure at the side point (V=55.56 m/s): $$p_2 = \tfrac{1}{2}(1.19)(27.78^2 - 55.56^2) = \tfrac{1}{2}(1.19)(-2314.8) = \boxed{-1377\ \text{Pa} = -1.377\ \text{kPa}}$$
LocationVelocityGauge pressure
Point 1 (front, stagnation)0 m/s+0.459 kPa
Point 2 (side, θ=90°)55.56 m/s−1.377 kPa (suction)