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22-Mec-B6 Advanced Fluid Mechanics · May 2014

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.

Question 4 (Part A, Question A4): Full-Similarity Water-Tunnel Testing of a Suspension-Bridge Deck (14 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.

QuantityPrototype (air)Model (water)
Characteristic lengthdeck length 50 m, width 5 m1/20 scale: 2.5 m, 0.25 m
Density \(\rho\)1.2 kg/m31000 kg/m3
Dynamic viscosity \(\mu\)18×10−6 Pa·s0.001 Pa·s
Kinematic viscosity \(\nu=\mu/\rho\)15×10−6 m2/s1×10−6 m2/s
Speed30 m/s (given)to be found
Measured lift / dragto be predicted1.0 MN / 0.1 MN
Oscillation frequencyto be predicted5 Hz

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.

Prototype (air)Model 1:20 (water tunnel)deck length 50 m, width 5 m30 m/srho = 1.2, nu = 15e-6 m^2/slift 270 kN, drag 27 kN, f = 0.1875 Hz2.5 m long, 0.25 m wide40 m/srho = 1000, nu = 1e-6 m^2/slift 1.0 MN, drag 0.1 MN, f = 5 Hzmatched Reynolds number Re = 1.0 × 10^8 ; matched Strouhal number St = 0.3125
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.

  1. 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.
  2. 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.
  3. 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.
  4. 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.
PartQuantityValue
(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 lift0.270 MN = 270 kN
(b)Full-scale drag0.0270 MN = 27 kN
(c)Common Strouhal number0.3125
(c)Full-scale oscillation frequency0.1875 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.