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22-Mec-B6 Advanced Fluid Mechanics · May 2014

Question 1 of 7: Question 1 (Part A, Question A1): Drag and Power for a Flat Plate Towed Edgewise

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 1 (Part A, Question A1): Drag and Power for a Flat Plate Towed Edgewise (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.

QuantitySymbolValue
Plate dimensions\(a \times b\)5 m × 1 m (planform area 5 m2)
Tow speed\(U_o\)15 m/s
Transition Reynolds number\(Re_{cr}\)500 000
Water\(\rho,\ \nu\)1000 kg/m3, 1×10−6 m2/s
Air\(\rho,\ \nu\)1.2 kg/m3, 15×10−6 m2/s
Aid-sheet laminar law\(C_{fx}\)\(0.67\,Re_x^{-1/2}\)
Aid-sheet turbulent law\(C_{fx}\)\(0.0266\,Re_x^{-1/7}\)

In arrangement A side a = 5 m is normal to the flow (it is the leading edge, as drawn in Fig. A1), so the stream runs only \(L = b = 1\ \text{m}\) along the plate over a width \(w = a = 5\ \text{m}\). In arrangement B side b = 1 m is the leading edge, so \(L = a = 5\ \text{m}\) and \(w = b = 1\ \text{m}\). The plate is thin, so both faces carry a boundary layer and the wetted area is \(2ab = 10\ \text{m}^2\) in either case.

Find. The towing force and the towing power for each arrangement in each fluid, which arrangement costs less power, and by what percentage.

Arrangement BArrangement AU_o = 15 m/sa = 5 m (streamwise, L)b = 1 mleading edge is the short sideL = 5 m, width w = 1 mU_o = 15 m/sb = 1 m (streamwise, L)a = 5 mleading edge is the long side, L = 1 m, w = 5 m
Figure 1.1 — The two towing arrangements. Only the streamwise length changes; the planform and wetted areas are identical.

Approach. Integrate the aid-sheet local skin-friction law along each face, splitting the integral at the transition point \(x_{tr}\) where \(Re_x = 5\times10^5\), to obtain a mean coefficient \(C_F\); then \(D = 2\left(\tfrac{1}{2}\rho U_o^2 wL\,C_F\right)\) and \(P = D\,U_o\).

  1. Locate the transition point in each fluid. Transition sits where \(Re_x = U_o x/\nu = Re_{cr}\), so \[x_{tr} = \frac{\nu\,Re_{cr}}{U_o}.\] In water \(x_{tr} = (10^{-6})(5\times10^{5})/15 = 0.0333\ \text{m}\); in air \(x_{tr} = (15\times10^{-6})(5\times10^{5})/15 = 0.500\ \text{m}\). This one number decides the whole question: in water transition happens within the first 3 cm of either plate, while in air it takes half a metre — which is half of the 1 m plate in arrangement B.
  2. Integrate the wall shear over one face. The drag on one face of width \(w\) is \(D_1=\int_0^L \tau_w(x)\,w\,dx\) with \(\tau_w = \tfrac{1}{2}\rho U_o^2 C_{fx}\). Defining the mean coefficient \(C_F = \frac{1}{L}\int_0^L C_{fx}\,dx\) and substituting the two aid-sheet laws, \[\begin{aligned}\int_0^{x_{tr}}\!\frac{0.67}{Re_x^{1/2}}\,dx&=\frac{1.34\,x_{tr}}{Re_{cr}^{1/2}},\\\int_{x_{tr}}^{L}\!\frac{0.0266}{Re_x^{1/7}}\,dx&=\frac{7}{6}(0.0266)\!\left[\frac{L}{Re_L^{1/7}}-\frac{x_{tr}}{Re_{cr}^{1/7}}\right].\end{aligned}\] Both integrals are elementary because \(Re_x\) is linear in \(x\); the \(7/6\) factor is the exponent bookkeeping of \(x^{-1/7}\).
  3. Evaluate the mean coefficient for each case. Adding the two contributions and dividing by \(L\) gives \[\boxed{C_F = \frac{1}{L}\left[\frac{1.34\,x_{tr}}{\sqrt{Re_{cr}}}+\frac{7}{6}(0.0266)\left(\frac{L}{Re_L^{1/7}}-\frac{x_{tr}}{Re_{cr}^{1/7}}\right)\right]}\] which yields the four values tabulated below. Note that arrangement B in water has \(Re_L = 7.5\times10^{7}\) — essentially an all-turbulent plate — whereas arrangement A in air is 50 per cent laminar.
  4. Convert to force and power. With both faces wetted, \[D = 2\cdot\tfrac{1}{2}\rho U_o^2\,(wL)\,C_F=\rho U_o^{2}\,(wL)\,C_F,\qquad P = D\,U_o .\] Because \(wL = 5\ \text{m}^2\) and \(U_o = 15\ \text{m/s}\) are the same in every case, the force ratio between arrangements is the \(C_F\) ratio.
FluidArrangement\(L\) (m)\(Re_L\)\(x_{tr}/L\)\(C_F\)\(D\) (N)\(P\)
(a) WaterB (b leading)57.50×1070.00670.0023082596.538.95 kW
A (a leading)11.50×1070.03330.0028333187.347.81 kW
(b) AirB (b leading)55.00×1060.1000.0031404.23963.58 W
A (a leading)11.00×1060.5000.0028793.88758.30 W

The two fluids give opposite answers, and that is the point of the question. In water the laminar run is negligible in both arrangements, so the only thing that matters is that a longer plate has a thicker, slower-growing turbulent layer and therefore a smaller mean coefficient: arrangement B wins. In air the laminar run is a full half of the short plate, and the laminar contribution is so much cheaper than the turbulent one that arrangement A wins despite its larger turbulent-layer growth rate. The plot below shows \(C_F(L)\) for both fluids with the two operating points marked.

0.001 0.002 0.003 0.004 0.005 water B A air B A A: L = 1 m B: L = 5 m U = 15 m/s, Re_cr = 5x10^5 1 2 3 4 5 6 streamwise plate length L (m) mean C_F (one face)
Figure 1.2 — Mean skin-friction coefficient versus streamwise plate length at \(U_o=15\) m/s. The water curve falls monotonically through both operating points; the air curve bottoms out at the all-laminar \(L=0.5\) m (where transition first appears), climbs to a peak near \(L\approx2.7\) m and falls only slowly beyond it, so the 1 m plate sits below the 5 m plate.
  1. Percentage power reduction, water. Arrangement B is the efficient one: \[\begin{aligned}\text{saving}&=\frac{P_A-P_B}{P_A}=\frac{47.81-38.95}{47.81}=0.1854\\&\Rightarrow\ \boxed{\text{arrangement B uses }18.5\text{ per cent less power}}\end{aligned}\]
  2. Percentage power reduction, air. Here arrangement A is the efficient one: \[\begin{aligned}\text{saving}&=\frac{P_B-P_A}{P_B}=\frac{63.58-58.30}{63.58}=0.0830\\&\Rightarrow\ \boxed{\text{arrangement A uses }8.3\text{ per cent less power}}\end{aligned}\]
ResultWaterAir
Transition point \(x_{tr}\)0.0333 m0.500 m
Drag, arrangement A (L = 1 m)3187.3 N3.887 N
Power, arrangement A (L = 1 m)47.81 kW58.30 W
Drag, arrangement B (L = 5 m)2596.5 N4.239 N
Power, arrangement B (L = 5 m)38.95 kW63.58 W
More efficient arrangementB (long side streamwise)A (short side streamwise)
Power reduction achieved18.5 per cent8.3 per cent

Check: modelling assumptions. The plate is treated as a zero-thickness flat plate at zero incidence, so only skin friction acts — no form drag, no edge (finite-width) effects, and no wave making at a free surface. Transition is taken as abrupt at \(Re_x = 5\times10^{5}\) rather than as a transition region, and the turbulent correlation is applied from \(x_{tr}\) as if the turbulent layer had started at the leading edge. The coefficients 0.67 and 0.0266 are the paper's own aid-sheet values; the more familiar textbook constants (0.664 laminar, 0.027 turbulent) would change the forces by well under one per cent.

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