Question 4 of 7: Question 4 (Part A, Question A4): Full-Similarity Water-Tunnel Testing of a Suspension-Bridge Deck
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, May 2014 — 07-Mec-B6
Advanced Fluid Mechanics. Three hours, open book, any non-communicating
calculator permitted. Part A holds four questions and the candidate answers any three of them
(42 per cent of the paper, so 14 marks each); Part B holds three questions and the
candidate answers any two (58 per cent, so 29 marks each). All seven questions
are worked here.
The paper supplies an aid sheet of compressible-flow, boundary-layer, Navier–Stokes and
potential-flow relations; the skin-friction coefficients used below are taken from that sheet
(not from the Blasius/White constants a textbook would give) so that the arithmetic
matches what a candidate had in front of them.
Reference texts.
F. M. White, Fluid Mechanics, 8th ed. — Ch. 5 (dimensional analysis and
similitude), Ch. 7 (external flow and plate drag), Ch. 8 (potential flow), Ch. 9 (compressible
flow, Fanno line, normal shocks).
F. M. White, Viscous Fluid Flow, 3rd ed. — Ch. 3 (exact solutions of the
Navier–Stokes equations, annular Couette flow), Ch. 6 (turbulent wall flow).
J. D. Anderson, Modern Compressible Flow, 3rd ed. — Ch. 3 (normal shock
waves), Ch. 5 (quasi-one-dimensional nozzle and diffuser flow).
P. K. Kundu, I. M. Cohen and D. R. Dowling, Fluid Mechanics, 6th ed. —
Ch. 6 (irrotational flow, method of images), Ch. 9 (laminar internal flow).
H. Schlichting and K. Gersten, Boundary-Layer Theory, 8th ed. — Ch. 21
(plate drag with a mixed laminar/turbulent boundary layer).
R. W. Fox, A. T. McDonald and J. W. Mitchell, Introduction to Fluid Mechanics,
10th ed. — Ch. 7 (similitude and model testing), Ch. 13 (compressible flow with
friction).
Question 4 (Part A, Question A4): Full-Similarity Water-Tunnel Testing of a Suspension-Bridge Deck (14 marks)
Find. (a) the water-tunnel speed that gives full similarity, (b) the full-scale
lift and drag implied by the measured model forces, and (c) the full-scale oscillation frequency.
Figure 4.1 — Model-to-prototype mapping. Reynolds similarity fixes
the tunnel speed; force and Strouhal coefficients then transfer the measured loads and frequency.
Approach. "Full similarity" for a bluff body in a single-phase flow means
matching the Reynolds number, which fixes the model speed; the force coefficient
\(F/(\rho V^2 L^2)\) and the Strouhal number \(fL/V\) are then equal between model and prototype and
transfer the measurements.
Part (a) — impose Reynolds similarity. Setting
\(Re_m=Re_p\) with \(\nu=\mu/\rho\),
\[\frac{V_m L_m}{\nu_m}=\frac{V_p L_p}{\nu_p}
\quad\Rightarrow\quad
V_m=V_p\left(\frac{L_p}{L_m}\right)\left(\frac{\nu_m}{\nu_p}\right).\]
The scale ratio is \(L_p/L_m=20\) and the viscosity ratio is
\(\nu_{\text{water}}/\nu_{\text{air}}=1\times10^{-6}/15\times10^{-6}=1/15\), so
\[V_m=(30)(20)\left(\tfrac{1}{15}\right)\]
\[\boxed{V_m=40\ \text{m/s}}\]
As a check, both Reynolds numbers on the deck length are
\(Re=(30)(50)/(15\times10^{-6})=(40)(2.5)/(1\times10^{-6})=1.0\times10^{8}\). Water is chosen
precisely because its low kinematic viscosity lets a 1/20 model reach full-scale \(Re\) at a
manageable speed; the same test in air would need 600 m/s and be hopelessly compressible.
Part (b) — transfer the forces through the force coefficient. Similarity
of \(C_F=F/(\rho V^2 L^2)\) gives
\[\begin{aligned}\frac{F_p}{F_m}&=\left(\frac{\rho_p}{\rho_m}\right)\left(\frac{V_p}{V_m}\right)^{2}\left(\frac{L_p}{L_m}\right)^{2}\\&=\left(\frac{1.2}{1000}\right)\left(\frac{30}{40}\right)^{2}(20)^{2}\\&=(1.2\times10^{-3})(0.5625)(400)=0.270 .\end{aligned}\]
The prototype loads are therefore smaller than the model loads, because the density ratio
of 1/833 overwhelms the 400-fold area ratio.
Evaluate the two forces. Applying the same factor to each measurement,
\[\begin{aligned}\boxed{L_p=(0.270)(1.0\ \text{MN})=0.270\ \text{MN}=270\ \text{kN}}\\\boxed{D_p=(0.270)(0.1\ \text{MN})=0.0270\ \text{MN}=27\ \text{kN}}\end{aligned}\]
The lift-to-drag ratio of 10 is of course preserved, since both forces scale identically.
Part (c) — transfer the frequency through the Strouhal number. Matching
\(St=fL/V\),
\[f_p=f_m\left(\frac{V_p}{V_m}\right)\left(\frac{L_m}{L_p}\right)=(5)\left(\frac{30}{40}\right)\left(\frac{1}{20}\right)\]
\[\boxed{f_p=0.1875\ \text{Hz}\quad(\text{period }5.33\ \text{s})}\]
The common Strouhal number is \(St=(5)(2.5)/40=(0.1875)(50)/30=0.3125\). A period of five seconds is
exactly the order of the torsional oscillation that destroyed the Tacoma Narrows bridge, which is
why this frequency — not the force — is usually the governing result of such a
test.
Part
Quantity
Value
(a)
Water-tunnel speed \(V_m\)
40 m/s
(a)
Common Reynolds number (deck length)
1.0×108
(b)
Force scale \(F_p/F_m\)
0.270
(b)
Full-scale lift
0.270 MN = 270 kN
(b)
Full-scale drag
0.0270 MN = 27 kN
(c)
Common Strouhal number
0.3125
(c)
Full-scale oscillation frequency
0.1875 Hz (5.33 s period)
Check: what "full similarity" can and cannot deliver.
Geometric similarity is assumed at 20:1 in every dimension, including deck details and cable
diameters, and the model is assumed rigid enough that its measured forces are not contaminated by
its own structural response. Reynolds matching alone is used because the flow is single-phase and
low-speed; if free-surface effects or gravity waves mattered, Froude similarity would also be
required and could not be satisfied simultaneously with Reynolds in the same fluid. Compressibility
is ignored in both streams (\(M_{\text{air}}=0.09\)) and cavitation in the water tunnel at 40 m/s is
assumed to be suppressed by adequate tunnel pressure.