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04-BS-7 · Undated paper

Question 6 of 13: Force, Power and Efficiency of a Jet on a Moving Curved Plate

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

Notes on this paper

04-BS-7 Mechanics of Fluids — undated sitting, identified as May 2019 (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.” A complete paper is any 10 of the 13, each worth 5 marks. Every question is answered below (13 of 13) so the set can be used as a full study resource. Constants used throughout (from the paper's own Constants page, p.12): g = 9.81 m/s², patm = 100 kPa, ρwater = 1000 kg/m³, SGbenzene = 0.90, SGmercury = 13.56, SGcarbon tetrachloride = 1.59, ρair = 1.19 kg/m³ (20°C), μwater = 1.0×10⁻³ N·s/m², μair = 1.8×10⁻⁵ N·s/m².

Reference texts: F. M. White, Fluid Mechanics, 8th ed. (McGraw-Hill) — fluid statics and manometry (Ch. 2), hydrostatic forces on plane surfaces (Ch. 2), the Bernoulli/continuity pair and orifice flow (Ch. 3), the linear-momentum equation for moving vanes (Ch. 3), pipe friction and the Moody/Colebrook relation (Ch. 6), boundary layers and drag (Ch. 7), capillary rise (Ch. 1), high-lift devices and aircraft wing aerodynamics (J. D. Anderson, Fundamentals of Aerodynamics, Ch. 4–5).

Question 6: Force, Power and Efficiency of a Jet on a Moving Curved Plate (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 speed, U10 m/s (same direction as jet)
Turning angle180°, frictionless
V1 = 30 m/s U = 10 m/s
Jet strikes the moving curved plate and is deflected 180°; the plate itself advances at U in the same direction as the incoming jet.

Approach. Work in the frame of the moving plate: the fluid approaches at relative velocity (V1−U) and leaves at the same relative speed reversed (180° turn, no friction), so the linear-momentum equation gives the force, and power follows from force × plate speed; efficiency compares that power to the kinetic-energy rate of the absolute jet.

  1. Part (a): force on the plate. Relative velocity V1−U = 20 m/s; only the mass flow that actually catches the moving plate matters, ρA(V1−U), and the momentum change per unit mass for a full 180° reversal is 2(V1−U): $$ F = \rho A (V_1-U)\big[2(V_1-U)\big] = 2\rho A (V_1-U)^2 $$ $$ F = 2(1000)\left(\tfrac{\pi}{4}(0.050)^2\right)(20)^2 $$ $$ \boxed{F \approx 1571\ \text{N}} $$
  2. Part (b): power developed. $$ P = F\,U = (1571)(10) $$ $$ \boxed{P \approx 15\,708\ \text{W}} $$
  3. Part (c): efficiency of energy transfer. Compare to the kinetic-energy rate of the absolute jet leaving the nozzle, $P_{in}=\tfrac12 \dot m V_1^2$ with ṁ=ρAV1: $$ \dot m = \rho A V_1 = (1000)(0.0019635)(30) \approx 58.9\ \text{kg/s} $$ $$ P_{in} = \tfrac12(58.9)(30)^2 \approx 26\,507\ \text{W} $$ $$ \eta = \frac{P}{P_{in}} = \frac{15\,708}{26\,507} $$ $$ \boxed{\eta \approx 59.3\%} $$
  4. Part (d): plate speed for maximum efficiency. Writing power as a function of U, $P(U)=2\rho A(V_1-U)^2U$, and setting dP/dU=0 gives 3U^2-4V_1U+V_1^2=0, whose non-trivial root is: $$ \boxed{U_{opt} = \frac{V_1}{3} = \frac{30}{3} = 10\ \text{m/s}} $$ This is exactly the plate speed given in parts (a)–(c) — the problem is set up at its own optimum. The physical reason: power is the product of a shrinking relative-velocity-squared term (which falls as U rises) and a growing U term; the classic single-moving-vane result balances these two competing trends at U = V1/3, beyond which the loss of relative momentum outweighs the gain in plate speed.
QuantityResult
Force on plate (U=10 m/s)1571 N
Power developed15.71 kW
Efficiency59.3%
Optimal plate speedU = V1/3 = 10 m/s