Difficulty: Medium
Correct Answer: F = ρ a V^2 sin θ
Explanation:
Given
Approach
Take x along the jet and y normal to the jet. The plate eliminates the normal-to-plate velocity component; in x–y, the outgoing flow has zero y-component.
Step-by-step
Incoming momentum flux in y = ṁ (V sin θ) = ρ a V · V sin θ = ρ a V^2 sin θ.Outgoing momentum flux in y = 0 (fixed plate, flow slides along the plate).Force on plate in +y (on fluid in −y) = Δ(momentum flux in y) = ρ a V^2 sin θ.
Checks
θ = 0° ⇒ F = 0 (plate parallel to flow) ✔θ = 90° ⇒ F = ρ a V^2 (plate normal to flow) ✔
Final Answer
F = ρ a V^2 sin θ
Discussion & Comments