04-BS-7 · Undated paper
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
04-BS-7 Mechanics of Fluids — undated sitting, identified as May 2019 (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.” A complete paper is any 10 of the 13, each worth 5 marks. Every question is answered below (13 of 13) so the set can be used as a full study resource. Constants used throughout (from the paper's own Constants page, p.12): g = 9.81 m/s², patm = 100 kPa, ρwater = 1000 kg/m³, SGbenzene = 0.90, SGmercury = 13.56, SGcarbon tetrachloride = 1.59, ρair = 1.19 kg/m³ (20°C), μwater = 1.0×10⁻³ N·s/m², μair = 1.8×10⁻⁵ N·s/m².
Reference texts: F. M. White, Fluid Mechanics, 8th ed. (McGraw-Hill) — fluid statics and manometry (Ch. 2), hydrostatic forces on plane surfaces (Ch. 2), the Bernoulli/continuity pair and orifice flow (Ch. 3), the linear-momentum equation for moving vanes (Ch. 3), pipe friction and the Moody/Colebrook relation (Ch. 6), boundary layers and drag (Ch. 7), capillary rise (Ch. 1), high-lift devices and aircraft wing aerodynamics (J. D. Anderson, Fundamentals of Aerodynamics, Ch. 4–5).
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.
Part (a) — Sketch and explanation. A pitot-static tube carries two concentric passages: the central, forward-facing tip senses the stagnation (total) pressure where the flow is brought to rest, while a ring of small side ports further back on the probe senses the undisturbed static pressure of the duct flow. Each passage is piped to one leg of a U-tube manometer containing water; because the duct fluid (air) is far less dense than the manometer fluid (water), the manometer deflection is small but readable, and the deflection is driven purely by the dynamic pressure of the flow.
Approach for (b) and (c). The manometer reading converts to the true dynamic pressure via Δp = (ρwater − ρair)gΔh, and that same dynamic pressure equals ½ρairV² by the pitot-static (Bernoulli) relation — so a direct-reading pressure gauge would show exactly the same Δp, just without the density-difference amplification a liquid column provides.
| Quantity | Result |
|---|---|
| Air velocity in duct | 19.9 m/s |
| Differential gauge reading | 0.235 kPa |