Question 4 of 6: Wall shear stress from a pipe force balance
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exams — December 2018 — 16-Civ-A5, Hydraulic Engineering. Closed book (one aid sheet; approved calculator); 3 hours; six questions, candidates complete any five — all six are solved here as a study resource. Each question 20 marks; parts of equal value.
Governing relations supplied on the exam cover sheet: Hazen–Williams $Q = 0.278\,C\,D^{2.63}\,S^{0.54}$ with slope $S=\Delta h/L$ (SI: $Q$ in m³/s, $D$ in m); Manning $Q=\tfrac{1}{n}A\,R^{2/3}\,S^{1/2}$; Darcy–Weisbach $\Delta h = 0.0826\,\tfrac{fL}{D^{5}}Q^{2}$; total dynamic head $TDH=H_s+H_f$. Unless stated, local losses and velocity head are negligible, diameters are nominal, and the fluid is water ($\rho=1000\ \text{kg/m}^3$, $\nu=1.31\times10^{-6}\ \text{m}^2/\text{s}$).
Question 4: Wall shear stress from a pipe force balance (20 marks)
Given. Steady, fully-developed flow in a horizontal circular pipe; pressure drop $\Delta P=15\ \text{kPa}$ over length $L=2\ \text{m}$; diameter $D=0.150\ \text{m}$ ($R=0.075\ \text{m}$).
Given data
Quantity
Value
Pressure difference $\Delta P$
15 kPa = 15,000 Pa
Length $L$
2 m
Diameter $D$ (radius $R$)
0.150 m (0.075 m)
Find. A regime-independent relation between wall shear stress $\tau_w$ and average velocity $V$, and the numerical $\tau_w$ for the stated data.
Figure 4. Free body of the fluid cylinder: pressure force drives flow; wall shear resists it.
Approach. Apply Newton’s second law to the cylindrical fluid core of radius $R$ and length $L$. In steady, fully-developed flow the momentum flux in equals out, so the net pressure force balances the wall shear force — a statement independent of whether the flow is laminar or turbulent. Then fold in the Darcy–Weisbach definition to express the same $\tau_w$ through the average velocity.
Force balance on the fluid cylinder. Pressure acts on the end area $\pi R^{2}$; shear acts on the lateral area $2\pi R L$:
$$(P_1-P_2)\,\pi R^{2}=\tau_w\,(2\pi R L).$$
Solve for wall shear. Cancelling and using $R=D/2$,
$$\boxed{\tau_w=\frac{\Delta P\,R}{2L}=\frac{\Delta P\,D}{4L}.}$$
This holds for any regime because it is pure statics — no constitutive (viscous) law was invoked.
Relate to average velocity. Darcy–Weisbach writes the same drop as $\Delta P=f\dfrac{L}{D}\dfrac{\rho V^{2}}{2}$. Substituting into $\tau_w=\Delta P\,D/4L$ gives the regime-independent form
$$\tau_w=\frac{f}{8}\,\rho V^{2},$$
with $f$ from the laminar law $64/Re$ or the Colebrook/Moody chart for turbulent flow.