Difficulty: Medium
Correct Answer: ρ a Vr (V − v)
Explanation:
Concept / Approach
Thrust in jet propulsion comes from the rate of change of momentum in the direction of motion.
Mass flow rate through the ship's system (as seen on the ship) = ρ a Vr.
Velocity component change along the ship's axis between inlet and exit = (V − v) − 0, because the inflow through side inlets has no axial component.
Step-by-step
Thrust F = (mass flow rate) × (axial velocity change) F = (ρ a Vr) × (V − v)
Verification
If the ship is stationary (v = 0), then Vr = V, and F reduces to ρ a V × V = ρ a V², as expected for a stationary nozzle.
Common pitfalls
Adding velocities instead of taking the difference (V − v) in the momentum change term. Using ρ a V instead of ρ a Vr for the mass flow seen by the moving ship.
Final Answer
ρ a Vr (V − v)
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