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18-Env-A2 Hydrology and Municipal Hydraulics Engineering · Undated paper

Question 5 of 7

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

Notes on this paper

National Exams — May 2019 — 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. 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.); Davis & Cornwell, Introduction to Environmental Engineering (6th ed.); Guidelines for Canadian Drinking Water Quality (Health Canada); Canadian Council of Ministers of the Environment (CCME) water-quality guidelines.

Problem 5 (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) Stage-discharge approach: derivation, use, and 25-year prediction parameters (7 marks)

Derivation and use. The stage-discharge (rating curve) approach relies on the fact that, at a stable, well-defined channel control (a natural constriction, riffle, or engineered weir/flume), discharge is a single-valued, repeatable function of stage: $Q=f(h)$. The relationship is established empirically by making periodic direct discharge measurements (current-meter or ADCP gauging) simultaneously with stage readings across a wide range of flows, then fitting a smooth curve (commonly a power-law form $Q=a(h-h_0)^b$, where $h_0$ is the stage of zero flow) through the paired $(h,Q)$ observations. Once established, the rating curve converts the CONTINUOUSLY recorded stage (from an automatic stage recorder, cheap and simple to operate continuously) into a continuous discharge record WITHOUT requiring a discharge measurement to be made at every time step — discharge measurement itself is comparatively labour-intensive and cannot be automated as easily as stage, which is exactly why the stage-discharge relationship is the practical bridge between continuously measurable stage and the discharge record actually needed for design and water-balance work.

Two key parameters affecting a 25-year streamflow prediction. (1) Channel control stability (bed/bank change over time). A rating curve is only valid as long as the control section's geometry is unchanged; channel aggradation/degradation, vegetation growth, ice effects, or a major flood that reshapes the control all shift the true $Q=f(h)$ relationship, so a rating curve established today can be significantly wrong 25 years later unless it is periodically re-verified with fresh discharge measurements (rating shifts are the dominant source of long-term streamflow-record error). (2) Land-use and climate change in the contributing watershed. Even with a perfectly stable control, the STAGE record itself (and hence the predicted discharge) reflects the watershed's runoff-generation behaviour at the time of measurement; over a 25-year horizon, urbanization (reduced infiltration, higher peak/lower baseflow), forestry/land clearing, and shifting precipitation patterns under climate change all alter the underlying rainfall-runoff relationship, so a stage-discharge-based prediction extrapolated 25 years forward implicitly assumes watershed conditions the gauge record may no longer represent unless it is explicitly adjusted for anticipated land-use/climate trends.

(ii) Trapezoidal channel: uniform-flow discharge and Reynolds number (6 marks)

Given.

QuantityValue
Normal depth, $y$2.5 m
Base width, $b$8 m
Side slope (H:V)1:4, i.e. $z=1/4=0.25$
Bed slope, $S_o$3% = 0.03
Manning's $n$ (finished concrete lining)0.013
b = 8 my = 2.5 mH:V = 1:4Concrete-lined trapezoidal channel (uniform flow)
Fig. 2 — Trapezoidal cross-section, $b=8$ m, $y=2.5$ m, side slopes 1:4 (H:V), i.e. steep, near-vertical concrete-lined banks.

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.$$A=(b+zy)y=(8+0.25\times2.5)(2.5)=\boxed{21.56\ \text{m}^2}\qquad P=b+2y\sqrt{1+z^2}=8+2(2.5)\sqrt{1.0625}=13.15\ \text{m}\qquad R=\frac{A}{P}=1.639\ \text{m}$$$$Q=\frac{1}{n}AR^{2/3}S_o^{1/2}=\frac{1}{0.013}(21.56)(1.639)^{2/3}(0.03)^{1/2}=\boxed{399.4\ \text{m}^3/\text{s}}=23964\ \text{m}^3/\text{min}$$
  2. Part (b) — Reynolds number.$$V=\frac{Q}{A}=\frac{399.4}{21.56}=18.52\ \text{m/s}\qquad Re=\frac{VR}{\nu}=\frac{(18.52)(1.639)}{1.0\times10^{-6}}=\boxed{3.036\times10^{7}}$$Since open-channel flow is turbulent for $Re\gtrsim12{,}500$ (hydraulic-radius Reynolds number), this flow is strongly turbulent.
QuantityValue
Flow area, $A$21.56 m²
Hydraulic radius, $R$1.639 m
Discharge, $Q$399.4 m³/s = 23964 m³/min
Reynolds number, $Re$$3.036\times10^{7}$ (turbulent)
Check: an H:V of 1:4 (steep, near-vertical banks) combined with a smooth $n=0.013$ finished-concrete lining and a 3% bed slope produces a very high velocity (18.52 m/s) for an open channel — this would in practice be a supercritical, air-entraining chute rather than ordinary "uniform flow," and would need chute/stilling-basin design rather than a simple trapezoidal-channel treatment. All three inputs (side slope, lining, and 3% slope) are taken exactly as printed on the exam and solved literally; the atypical result is flagged here rather than silently substituting a "nicer" value.

(iii) Specific energy over a bed rise, Q = 50 m³/s (7 marks)

Y₁ = 2.5 mY₂ = Y_c = 1.559 mΔz=0.6 mSection 1Crest (choked, Y=Y_c)flow
Fig. 3 — Longitudinal profile of the bed rise $\Delta z=0.6$ m; same trapezoidal cross-section ($b=8$ m, $z=0.25$) as part (ii). The upstream approach depth $Y_1=2.5$ m carries very little spare specific energy, so this bump chokes the flow.

Given. $Q=50\ \text{m}^3/\text{s}$, $Y_1=2.5$ m, bed rise $\Delta z=0.6$ m, same trapezoidal section ($b=8$ m, $z=0.25$); frictional losses negligible.

Find. Depth $Y_2$ at the raised section.

Approach. With no friction loss, specific energy referenced to the local bed falls by exactly $\Delta z$ across the rise, $E_2=E_1-\Delta z$. Before solving for $Y_2$, the crossing must be checked against the minimum specific energy (critical-flow) condition — if $\Delta z$ exceeds the available margin $E_1-E_{\min}$, no subcritical $Y_2$ exists and the crossing is choked.

  1. Approach conditions at Section 1.$$A_1=(8+0.25\times2.5)(2.5)=21.56\ \text{m}^2\qquad V_1=\frac{50}{21.56}=2.319\ \text{m/s}\qquad E_1=Y_1+\frac{V_1^2}{2g}=2.5+0.274=\boxed{2.774\ \text{m}}$$$$\text{Froude number: } Fr_1=\frac{Q}{A_1\sqrt{gA_1/T_1}}=0.485<1\ \ (\text{subcritical})$$
  2. Check whether the bump chokes the flow. Solving $Q^2T/(gA^3)=1$ numerically for the critical depth of this trapezoidal section gives $Y_c=1.559$ m, with minimum specific energy $E_{\min}=2.304$ m. The available margin is only$$\Delta z_{\max}=E_1-E_{\min}=2.774-2.304=0.470\ \text{m}$$Since the actual rise $\Delta z=0.6\ \text{m}>\Delta z_{\max}=0.470\ \text{m}$, the crossing is choked — no subcritical depth satisfies $E_2=E_1-\Delta z$ at this upstream depth.
  3. Depth at the raised section. A choked crossing is forced through critical depth at its highest point (the flow cannot carry more energy deficit than $E_1-E_{\min}$, so the free surface adjusts until the crest itself runs at critical depth):$$\boxed{Y_2=Y_c=1.559\ \text{m}}$$
  4. What actually happens upstream (afflux). Since $Y_1=2.5$ m cannot supply enough specific energy to clear a 0.6 m rise, water backs up until the approach section itself carries the higher specific energy $E_1'=E_{\min}+\Delta z=2.304+0.6=2.904$ m. Solving $E_1'=Y_1'+Q^2/(2gA(Y_1')^2)$ on the subcritical branch:$$Y_1'=\boxed{2.665\ \text{m}}$$i.e., the stated $Y_1=2.5$ m upstream depth is not sustainable once the 0.6 m bump is in place — the channel backs up (afflux) to about 2.665 m upstream of the rise before flow can pass over the crest at critical depth.
QuantityValue
Specific energy at Section 1 (at stated $Y_1=2.5$ m), $E_1$2.774 m
Critical depth for $Q=50$ m³/s, $Y_c$1.559 m
Available margin, $E_1-E_{\min}$0.470 m (< $\Delta z=0.6$ m → choked)
Depth at the raised section, $Y_2$1.559 m (= $Y_c$)
Required upstream depth to actually clear the hump, $Y_1'$2.665 m