04-BS-7 · December 2016
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
04-BS-7 Mechanics of Fluids — December 2016 (National Examinations, three hours, closed book). Section A (Calculative) offers 9 questions and instructs "do seven"; Section B (Graphical and 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, patm = 100 kPa, ρwater = 1000 kg/m³, ρconcrete = 2400 kg/m³, ρair = 1.19 kg/m³ (20°C) / 1.21 kg/m³ (15°C), μwater = 1.0×10⁻³ N·s/m², μair = 1.8×10⁻⁵ N·s/m², Rair = 287 J/kg·K.
Reference texts: F. M. White, Fluid Mechanics, 8th ed. (McGraw-Hill) — fluid statics and buoyancy/stability (Ch. 2), Bernoulli and control-volume momentum (Ch. 3), potential (inviscid) flow past a cylinder (Ch. 8), pipe friction and the Moody/Colebrook relation (Ch. 6), open-channel flow (Ch. 10), drag on immersed bodies and Stokes' law (Ch. 7); B. R. Munson et al., Fundamentals of Fluid Mechanics — actuator-disk propeller theory and variable-area tank draining.
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. The attached streamline diagram shows streamlines converging (bunching closer together) as they pass over the top of the cylinder, with the tightest spacing directly above the centre (90° from the front stagnation point), and re-diverging to their free-stream spacing by the rear (180°).
Find. V/V0 at ≥ 9 points from 0° to 180°, and the theoretical shape of the curve.
Approach. For steady, incompressible, inviscid flow, continuity between two streamlines requires V1b1 = V2b2 (equal volume flow per unit streamline spacing b); measuring the streamline spacing at the free stream and again at each angle θ around the cylinder converts the diagram directly into a velocity ratio, which for this classic geometry converges on the closed-form potential-flow result.
| θ (deg) | 0 | 22.5 | 45 | 67.5 | 90 | 112.5 | 135 | 157.5 | 180 |
|---|---|---|---|---|---|---|---|---|---|
| V/V0 = 2 sin θ | 0.000 | 0.765 | 1.414 | 1.848 | 2.000 | 1.848 | 1.414 | 0.765 | 0.000 |
Why the plot has this shape. At the front (0°) and rear (180°) stagnation points the flow must divide/rejoin, so the local velocity is zero and the streamline spacing equals the undisturbed spacing. Moving toward the shoulder, the cylinder blocks an increasing share of the flow area between adjacent streamlines, so by continuity they must bunch together and accelerate; the effect peaks at 90°, where the cylinder presents its full blocking width, giving the observed symmetric hump shape reaching 2V0.
| Quantity | Result |
|---|---|
| V/V0 at the front/rear stagnation points | 0 |
| V/V0 at the 90° shoulder (maximum) | 2.00 |
| Governing relation | V/V0 = 2 sin θ |