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04-BS-7 · May 2015

Question 6 of 13: Thrust on a Wind Turbine (Actuator-Disk Theory)

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

Notes on this paper

04-BS-7 Mechanics of Fluids — May 2015 (National Examinations, three hours, closed book). Section A (Calculative) offers 9 questions and instructs "do seven"; Section B (Analytical) offers 4 questions and instructs "do three." Every question is answered below (13 of 13), so students can use the full paper as a study resource.

Reference texts: F. M. White, Fluid Mechanics, 8th ed. (McGraw-Hill) — fluid statics (Ch. 2), the linear-momentum and energy equations (Ch. 3), pipe friction and the Moody chart (Ch. 6), and drag on immersed bodies (Ch. 7).

Question 6: Thrust on a Wind Turbine (Actuator-Disk Theory) (5 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.

QuantityValue
Free-stream wind speed, V₁10 m/s
Air density1.2 kg/m³
Turbine (disk) diameter4 m
Streamtube diameter, far upstream3 m
Streamtube diameter, far downstream4.5 m

Find. The thrust (axial force) the wind exerts on the turbine.

turbine diskV₁=10.0 m/sV_d=5.62V₂=4.44 m/sD₁=3.0 mD=4.0 mD₂=4.5 mThrust = 471.2 N
Fig. Q6 — the streamtube widens as it slows: smallest far upstream (undisturbed speed), largest far downstream (wake), matching mass conservation along the tube.

Approach. Apply mass conservation along the streamtube to get the velocity at the disk and far downstream, then apply the linear-momentum theorem over the whole tube (pressure is atmospheric at both open ends, so only the momentum flux terms survive).

  1. Continuity along the streamtube (same mass flow at every station): $$A_1V_1=A_{disk}V_{disk}=A_2V_2$$
  2. Velocity at the disk: $$V_{disk}=V_1\frac{A_1}{A_{disk}}=V_1\left(\frac{D_1}{D_{disk}}\right)^2=10\left(\frac{3}{4}\right)^2=\boxed{5.625\ \text{m/s}}$$
  3. Velocity far downstream: $$V_2=V_1\left(\frac{D_1}{D_2}\right)^2=10\left(\frac{3}{4.5}\right)^2=4.44\ \text{m/s}$$
  4. Mass flow rate through the disk (this is the mass flow for the whole tube): $$\dot m=\rho A_{disk}V_{disk}=1.2\left(\frac{\pi}{4}(4)^2\right)(5.625)=84.82\ \text{kg/s}$$
  5. Momentum theorem on the streamtube control volume (atmospheric pressure cancels at the two open ends; the turbine reaction force equals the momentum lost by the air): $$F=\dot m (V_1-V_2)=84.82(10-4.44)=\boxed{471\ \text{N}}$$
QuantityResult
Velocity at the disk5.63 m/s
Velocity far downstream4.44 m/s
Mass flow rate84.8 kg/s
Thrust on the turbine471 N