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04-BS-7 · December 2017

Question 8 of 13: Car Drag Coefficient, Power, and Fuel Consumption

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

Notes on this paper

04-BS-7 Mechanics of Fluids — National Examination, 2017-Dec. Three (3) hours duration, closed book. Section A (Calculative, 9 questions, do 7) and Section B (Graphical & Analytical, 4 questions, do 3); every question is answered below regardless of the exam's "do N of M" instruction, so the set is a complete study resource.

Reference texts: White, F.M., Fluid Mechanics (8th ed.) — fluid statics and manometry (Ch. 2), Bernoulli and flow measurement (Ch. 3), viscous flow in ducts and the Moody chart (Ch. 6), flow past immersed bodies and drag (Ch. 7), turbomachinery and wind turbines (Ch. 11).

Check — assumptions used across this paper:
  • Q1's manometer is read from the printed figure as a benzene(hatched)–mercury(black)–carbon-tetrachloride(clear) chain: benzene fills pipe A up and over the first bend and down the U-tube's left arm to the benzene/mercury interface at the UPPER dimension line (2.0 m + 400 mm = 2.4 m above A); the mercury stands 400 mm lower in the right arm, at the mercury/CCl₄ interface on the LOWER line (2.0 m above A); CCl₄ then fills the rest of the run over the second bend down to B, 3.0 m below A. (The mercury is higher on the A side, so pA < pB.)
  • Q6's spillway/gate width is read from the drawing as the 8.76 m dimension (the question's own hint: "width of each gate is slightly greater than its height" – 8.76 m > 8.23 m); the closed gate's wetted height at F.S.L. is F.S.L. − Crest = 7.92 m (the gate's own 8.23 m height extends slightly above F.S.L., matching the paper's note that "the top of the gate is higher than F.S.L.").
  • Q7 and Q9's friction/drag coefficients come from the Colebrook–White equation and the plotted drag curve — the same relations the attached Moody and drag charts plot.
  • Q9's Reynolds number (≈5.9×107) is beyond the attached drag chart's plotted range (10−1 to 106); CD = 0.3 is taken from the right-hand end of the cylinder curve (minimum ≈0.3 past the drag crisis, ≈0.33 at 106) — the best available reading — and flagged here as an extrapolation.
  • Q8(c)'s fuel density (needed to convert a fuel mass into litres) is not stated in Q8 itself; the paper lists no fuel density on its Constants page, so the gasoline SG = 0.75 given in Q4 of this same paper is adopted (Q2's 0.72 would give 3.50 L/100 km instead of 3.36).

Question 8: Car Drag Coefficient, Power, and Fuel Consumption (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
Wind (test/road) speed100 km/h = 27.78 m/s
Measured drag force, $F_D$302 N
Frontal area, $A$2.068 m²
Air density (20°C, Constants)1.19 kg/m³
Engine/transmission efficiency30%
Fuel calorific value40,000 kJ/kg
wind tunnel, V = 27.78 m/s F₀ = 302 N
Full-scale wind-tunnel test: drag force measured on the mounting scale at V = 100 km/h.

Find. (a) $C_D$; (b) power to overcome wind resistance; (c) fuel consumption (L/100 km) due to wind resistance alone.

Approach. (a) Invert the drag equation for $C_D$. (b) Power = force × velocity. (c) Convert power to fuel energy via the efficiency and calorific value, then to volume via the fuel density.

  1. (a) Drag coefficient. $$C_D=\frac{F_D}{\tfrac12\rho V^2A}=\frac{302}{\tfrac12(1.19)(27.78)^2(2.068)}=\frac{302}{949.6}=\boxed{0.318}$$
  2. (b) Power to overcome wind resistance. $$P=F_DV=(302)(27.78)=\boxed{8389\ \text{W} \approx 8.39\ \text{kW}}$$
  3. (c) Fuel power and energy for 100 km at 100 km/h (1.0 h = 3600 s). $$P_{fuel}=\frac{P}{\eta}=\frac{8389}{0.30}=27{,}963\ \text{W}\qquad E_{fuel}=P_{fuel}\times3600\ \text{s}=100.7\ \text{MJ}$$
  4. (c) Mass and volume of fuel. Using the calorific value and a gasoline density of SG 0.75 (the value this paper gives in Q4; no fuel density is listed on the Constants page): $$m_{fuel}=\frac{E_{fuel}}{CV}=\frac{100.7\times10^6}{40{,}000\times10^3}=2.52\ \text{kg}\qquad V_{fuel}=\frac{m_{fuel}}{\rho_{fuel}}=\frac{2.52}{750}=3.36\times10^{-3}\ \text{m}^3$$ $$\boxed{\approx 3.36\ \text{L per 100 km, due to wind resistance alone}}$$
QuantityValue
(a) Drag coefficient, $C_D$0.318
(b) Wind-resistance power8.39 kW
(c) Fuel consumption3.36 L/100 km