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18-Env-A2 Hydrology and Municipal Hydraulics Engineering · December 2018

Question 3 of 7

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

Notes on this paper

National Exams — December 2018 — 18-Env-A2 / Hydrology and Municipal Hydraulics Engineering. 3 hours duration; closed book with an 8.5×11 in double-sided aid sheet; Casio or Sharp approved calculator only. Any five questions constitute a complete paper (only the first five answers in the work book are marked); all seven Problems are solved below for completeness. Each question is worth 20 marks.

Reference texts. Davis & Cornwell, Introduction to Environmental Engineering (6th ed.); Linsley, Kohler & Paulhus, Hydrology for Engineers (3rd ed.); Chow, Open-Channel Hydraulics; Walski et al., Advanced Water Distribution Modeling and Management; Metcalf & Eddy, Wastewater Engineering: Treatment and Resource Recovery (5th ed.); Guidelines for Canadian Drinking Water Quality (Health Canada); Canadian Council of Ministers of the Environment (CCME) water-quality guidelines.

Problem 3 (20 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.

(i) Plastic pipe: flow rate, Reynolds number, head loss (6 marks)

Given.

QuantityValue
Length, $L$1000 m
Diameter, $d$500 mm = 0.500 m
Full-flow velocity, $V$4 m/s
Pipe materialplastic (PVC), $\varepsilon\approx1.5\times10^{-6}\ \text{m}$
Kinematic viscosity, $\nu$ (water, 20 °C)$1.004\times10^{-6}\ \text{m}^2/\text{s}$

Find. (a) $Q$ in m³/min; (b) $Re$ and flow type; (c) $H_f$ in m.

Approach. $Q$ from continuity; classify with $Re$; solve Colebrook–White for $f$ and apply Darcy–Weisbach.

  1. Part (a) — flow rate. $$A=\frac{\pi d^2}{4}=\frac{\pi(0.500)^2}{4}=0.1963\ \text{m}^2\qquad Q=VA=(4)(0.1963)=0.7854\ \text{m}^3/\text{s}=\boxed{47.12\ \text{m}^3/\text{min}}$$
  2. Part (b) — Reynolds number. $$Re=\frac{Vd}{\nu}=\frac{(4)(0.500)}{1.004\times10^{-6}}=\boxed{1.99\times10^{6}}$$ Since $Re\gg4000$, the flow is turbulent.
  3. Part (c) — friction head loss. Relative roughness $\varepsilon/d=3.0\times10^{-6}$ (hydraulically smooth plastic). Solving Colebrook–White iteratively gives $f=0.0105$. Applying Darcy–Weisbach: $$H_f=f\frac{L}{d}\frac{V^2}{2g}=(0.0105)\left(\frac{1000}{0.500}\right)\frac{(4)^2}{2(9.81)}=\boxed{17.11\ \text{m}}$$
QuantityValue
Flow rate, $Q$47.12 m³/min
Reynolds number, $Re$1.99×10&sup6; (turbulent)
Friction head loss, $H_f$17.11 m

(ii) Trapezoidal grass channel: uniform-flow discharge and Reynolds number (7 marks)

Given.

QuantityValue
Normal depth, $y$5 m
Base width, $b$4 m
Side slope (H:V)1:4, i.e. $z=0.25$
Bed slope, $S_o$3% = 0.03
Manning's $n$ (short grass, well maintained)0.030

Find. (a) Discharge $Q$; (b) Reynolds number and flow type.

Approach. Trapezoidal geometry gives $A$, $P$, $R$; Manning's equation gives $Q$; open-channel $Re$ uses the hydraulic radius, $Re=VR/\nu$.

  1. Part (a) — geometry and discharge. $$A=(b+zy)y=(4+0.25\times5)(5)=\boxed{26.25\ \text{m}^2}\qquad P=b+2y\sqrt{1+z^2}=4+2(5)\sqrt{1.0625}=14.31\ \text{m}\qquad R=\frac{A}{P}=1.835\ \text{m}$$ $$Q=\frac{1}{n}AR^{2/3}S_o^{1/2}=\frac{1}{0.030}(26.25)(1.835)^{2/3}(0.03)^{1/2}=\boxed{227.1\ \text{m}^3/\text{s}}$$
  2. Part (b) — Reynolds number. $$V=\frac{Q}{A}=\frac{227.1}{26.25}=8.65\ \text{m/s}\qquad Re=\frac{VR}{\nu}=\frac{(8.65)(1.835)}{1.004\times10^{-6}}=\boxed{1.58\times10^{7}}$$ Since open-channel flow is turbulent for $Re\gtrsim12{,}500$ (hydraulic-radius Reynolds number), this flow is strongly turbulent.
QuantityValue
Flow area, $A$26.25 m²
Hydraulic radius, $R$1.835 m
Discharge, $Q$227.1 m³/s
Reynolds number, $Re$1.58×10&sup7; (turbulent)
Check: a 1:4 (H:V) side slope is unusually steep for a grass-lined channel (most vegetated channels use $z\ge2$ for mowability/stability); it is taken as printed on the exam, consistent with this subject's established convention of solving with the literal given data and flagging an unusual value rather than silently "correcting" it.

(iii) Specific energy over a bed rise (7 marks)

Y₁Y₂ΔzSection 1Section 2 (crest)flow
Fig. 3 — Longitudinal profile of the channel bed rising by $\Delta z$ between Section 1 (upstream, depth $Y_1$) and Section 2 (crest, depth $Y_2$); same trapezoidal cross-section ($b=4$ m, $z=0.25$) as part (ii).

Given. $Q=10\ \text{m}^3/\text{s}$, $Y_1=2.5$ m, bed rise $\Delta z=0.5$ m, same trapezoidal section ($b=4$ m, $z=0.25$); frictional losses negligible.

Find. Depth $Y_2$ at the crest.

Approach. With no friction loss, total energy head is conserved along the channel, so the specific energy at the crest is $E_2=E_1-\Delta z$ (specific energy is referenced to the LOCAL bed). Check the crossing is not choked ($E_2\ge E_{\min}$ at critical depth) before solving the subcritical root of $E_2=Y_2+Q^2/(2gA(Y_2)^2)$.

  1. Approach conditions at Section 1. $$A_1=(4+0.25\times2.5)(2.5)=11.56\ \text{m}^2\qquad V_1=\frac{10}{11.56}=0.865\ \text{m/s}\qquad E_1=Y_1+\frac{V_1^2}{2g}=2.5+0.038=\boxed{2.538\ \text{m}}$$
  2. Check the bump does not choke the flow. Solving $Q^2T/(gA^3)=1$ numerically for the critical depth of this trapezoidal section gives $Y_c=0.845$ m, with minimum specific energy $E_{\min}=Y_c+A_c/(2T_c)=1.248$ m. Since $E_2=E_1-\Delta z=2.538-0.5=2.038\ \text{m} > E_{\min}=1.248\ \text{m}$, the crossing is not choked and a subcritical depth $Y_2$ exists at the crest.
  3. Solve for $Y_2$ on the subcritical branch ($Y_2>Y_c$). Solving $E_2=Y_2+Q^2/(2gA(Y_2)^2)=2.038$ m numerically (subcritical root): $$\boxed{Y_2=1.973\ \text{m}}$$ As expected for subcritical approach flow over a bump, the depth drops from $Y_1=2.5$ m to $Y_2=1.973$ m as the bed rises — the free surface itself dips by $Y_1-(Y_2+\Delta z)=2.5-2.473=0.027$ m over the crest.
QuantityValue
Specific energy at Section 1, $E_1$2.538 m
Critical depth, $Y_c$ (this $Q$)0.845 m
Depth at crest, $Y_2$1.973 m