Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exams — December 2013 — 04-Agric-A4, Fluid Flow. Three-hour, open-book exam; a Casio or Sharp approved calculator is permitted. Format: four questions constitute a complete paper, with a choice between 1a/1b and between 4a/4b; all questions require calculation. Both alternatives are solved below for completeness.
Reference texts: White, Fluid Mechanics (7th/8th ed., McGraw-Hill) — open-channel hydraulics (hydraulic jump, gradually varied flow over a bump), pipe friction (Colebrook–White), rotating control volumes (sprinkler reaction), and turbomachinery (pump performance curves, affinity laws).
Given. A three-arm sprinkler with frictionless (negligible collar) bearing, total flow $Q=2.7\ \text{m}^3/\text{hr}$ split equally among the three arms, arm radius $R=15\ \text{cm}$, nozzle diameter $d=7\ \text{mm}$, nozzle jet angled at $\theta$ measured from the tangent to the arm's circular path.
Quantity
Value
Total flow, $Q$
2.7 m³/hr = $7.5\times10^{-4}$ m³/s
Number of arms
3 (equal split)
Arm radius, $R$
0.15 m
Nozzle diameter, $d$
7 mm
Water
20°C, negligible collar friction
Find. The steady (free-wheeling) rotation rate $\omega$, in rev/min, for (a) $\theta=0^\circ$ and (b) $\theta=40^\circ$.
Figure 2 — Top view of the three-arm sprinkler: each nozzle exits at angle $\theta$ from the tangent to the R = 15 cm circle; the tangential component of the relative jet drives the rotation.
Approach. With collar friction negligible, the sprinkler spins up until the net torque is zero, i.e. until the absolute tangential velocity of the exiting jet is zero. Get the nozzle's relative exit speed from continuity per arm, then set the tangential component of that relative velocity equal to the tip speed $\omega R$.
Relative jet speed at each nozzle. Each of the 3 arms carries one third of the total flow through a nozzle of area $a=\tfrac{\pi}{4}d^2$:
$$q_{\text{arm}} = \frac{Q}{3} = \frac{7.5\times10^{-4}}{3} = 2.5\times10^{-4}\ \text{m}^3/\text{s}, \qquad a = \frac{\pi}{4}(0.007)^2 = 3.849\times10^{-5}\ \text{m}^2,$$
$$V_{\text{rel}} = \frac{q_{\text{arm}}}{a} = \frac{2.5\times10^{-4}}{3.849\times10^{-5}} = \boxed{V_{\text{rel}} \approx 6.50\ \text{m/s}}.$$
Torque-free (free-wheeling) condition. The angular-momentum flux gives a driving torque $T=\rho Q R\big(V_{\text{rel}}\cos\theta-\omega R\big)$ (per White's rotating-sprinkler control volume). With zero collar friction, steady state requires $T=0$, i.e. the jet's absolute tangential velocity vanishes:
$$V_{\text{rel}}\cos\theta = \omega R \;\Rightarrow\; \omega = \frac{V_{\text{rel}}\cos\theta}{R}.$$
(b) $\theta=40^\circ$.
$$\omega = \frac{6.50(\cos 40^\circ)}{0.15} = \frac{6.50(0.766)}{0.15} = 33.17\ \text{rad/s} \;\Rightarrow\; \boxed{n \approx 316.8\ \text{rev/min}}.$$
Angling the jets toward the tangent ($\theta$ up from $0^\circ$) reduces the tangential thrust component and so lowers the free-spin speed.