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Jet on hinged plate, force and angle

Short answer

Applied force at bottom to hold vertical plate is P = F/2 = 2454 N (about 2.45 kN). If force removed, equilibrium angle satisfies sinθ = ρaV²/W = 4908.7/W; e.g., 29.4° for a 10 kN plate weight.

A jet of the water, 50 mm in diameter, is striking normally with velocity of 50 m/s at the center of the plate which is hinged at its top edge and a horizontal external force is applied at the bottom edge to keep it vertical. What should be the amount of the applied force? If the force is removed what will be the angle of inclination of the plate with vertical for equilibrium condition?

Given: jet d=50d = 50 mm, V=50V = 50 m/s, a=π4(0.05)2=1.9635×10−3a = \dfrac{\pi}{4}(0.05)^2 = 1.9635\times 10^{-3} m². The plate is hinged at the top, and the jet strikes it normally at its centre.

Force required to hold the plate vertical

Force of the jet on the plate (normal to a flat plate at rest):

F=ρaV2=1000×1.9635×10−3×502=4908.7 NF = \rho aV^2 = 1000\times 1.9635\times 10^{-3}\times 50^2 = 4908.7\ \text{N}

This acts at the centre (distance L/2L/2 from the hinge, where LL is the plate length). Taking moments about the hinge, with the horizontal force PP applied at the bottom edge (distance LL):

P×L=F×L2  ⇒  P=F2=2454.4 NP\times L = F\times\frac{L}{2}\;\Rightarrow\; P = \frac{F}{2} = 2454.4\ \text{N}

Angle of inclination when the force is removed

If the force PP is removed, the plate swings out by an angle θ\theta from the vertical. Equilibrium requires the moment of the jet force about the hinge to equal the moment of the plate weight WW (acting at the plate's centre of gravity, L/2L/2 from the hinge).

The jet strikes at a distance ℓ\ell along the plate from the hinge, with ℓcos⁡θ=L/2\ell\cos\theta = L/2 (jet at fixed height). The normal force on an inclined plate is Fcos⁡θF\cos\theta (the jet makes angle 90∘−θ90^\circ - \theta with the plate).

Fcos⁡θ×L2cos⁡θ=W×L2sin⁡θ  ⇒  sin⁡θ=FW=ρaV2WF\cos\theta\times\frac{L}{2\cos\theta} = W\times\frac{L}{2}\sin\theta\;\Rightarrow\;\sin\theta = \frac{F}{W} = \frac{\rho aV^2}{W}

The weight WW of the plate is needed and is not given. For example, if W=10W = 10 kN: sin⁡θ=4908.7/10000=0.4909\sin\theta = 4908.7/10000 = 0.4909, so θ=29.4∘\theta = 29.4^\circ. If the plate weight is neglected, nothing resists the jet and the plate would swing up towards the horizontal (θ→90∘\theta \to 90^\circ).

Answer: applied force P=F/2=2454≈2.45P = F/2 = 2454 \approx 2.45 kN; the angle follows from sin⁡θ=ρaV2/W=4908.7/W\sin\theta = \rho aV^2/W = 4908.7/W (e.g. 29.4∘29.4^\circ for W=10W = 10 kN).

✓ Answer checked by Claude Opus 5.5 (high effort)

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