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04-BS-7 · December 2014

Question 5 of 13: Jet on a Moving Curved Plate (180° Turn)

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

Notes on this paper

04-BS-7 Mechanics of Fluids — National Examinations, December 2014. Three (3) hours, closed book. Section A: Calculative (9 questions, do 7); Section B: Analytical/Graphical (4 questions, do 3). Ten questions constitute a complete paper (50 marks). Every printed question is solved below, including the two "extra" questions in each Section beyond the minimum required.

Reference texts: White, Fluid Mechanics, 8th ed. (fluid statics & buoyancy Ch.2; Bernoulli/energy & momentum equations Ch.3; pipe friction & the Moody chart Ch.6; drag on immersed bodies Ch.7).

Question 5 — Jet on a Moving Curved Plate (180° Turn) (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
Jet diameter, d50 mm
Jet velocity, V130 m/s
Plate deflection180°, frictionless, moving with the jet

Find. (a) U for maximum efficiency; (b) force F on the plate; (c) power P developed; (d) efficiency η.

V1 = 30 m/s U plate moves in the SAME direction as the jet
Fig. Q5 — jet of speed V1 strikes a curved (bucket-like) plate moving at U in the same direction; the flow leaves reversed (180° turn) relative to the plate.

Approach. Work in the frame moving with the plate: the relevant relative velocity is Vr = V1 − U, and only the relative mass flow (ρA·Vr) participates in momentum exchange. Maximising the power-efficiency ratio over U gives the classic single-vane result.

  1. (a) Plate speed for maximum efficiency. The efficiency η(U) = 4U(V1−U)/V12 is maximised where dη/dU = 0, i.e. at the midpoint of the parabola: $$U = \frac{V_1}{2} = \frac{30}{2} = \boxed{15.0\text{ m/s}}$$
  2. (b) Force on the plate. Relative velocity Vr = 30−15 = 15 m/s; jet area A = π(0.050)²/4 = 1.9635×10−3 m²; relative mass flow ṁrel = ρAVr = 29.45 kg/s. A full 180° turn reverses the relative velocity, so ΔVrel = 2Vr: $$F = \dot m_{rel}(2V_r) = 29.45\times 2(15) = \boxed{883.6\text{ N}}$$
  3. (c) Power developed. $$P = FU = 883.6\times 15 = \boxed{13.25\text{ kW}}$$
  4. (d) Efficiency of energy transfer. Compared against the full kinetic power carried by the jet itself: $$P_{jet} = \tfrac{1}{2}\rho A V_1^3 = \tfrac{1}{2}(1000)(1.9635\times10^{-3})(30)^3 = 26.51\text{ kW}$$ $$\eta = \frac{P}{P_{jet}} = \frac{13.25}{26.51} = \boxed{50.0\%}$$
QuantityResult
(a) Optimum plate speed, U15.0 m/s
(b) Force, F883.6 N
(c) Power, P13.25 kW
(d) Efficiency, η50.0%