Determine the power of the jet engine of an airplane

AI Thread Summary
To determine the power of a jet engine, the discussion focuses on the mass flow rates of air and fuel, with air intake at 130 kg/s and fuel at 4.3 kg/s. The exit speed of the burned gases is 600 m/s, while the plane's speed is 260 m/s. The initial attempt to calculate power using the formula W = v^2(DM/DT) was deemed incorrect due to misunderstanding the application of momentum principles. The conversation emphasizes the need to apply Newton's second law correctly, particularly when mass is not constant. Ultimately, the correct approach involves analyzing the force as the rate of change of momentum.
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Homework Statement


The jet engine of an airplane takes in 130 kg of air per second, which is burned with 4.3 kg of fuel per second. The burned gases leave the plane at a speed of 600 m/s (relative to the plane). If the plane is traveling 260 m/s, determine the power (hp) delivered.


Homework Equations


P=Fv
M(DV/DT)=F_ext + v_rel(DM/DT)



The Attempt at a Solution


dv/dt=0 so F=v_rel(DM/DT)
Thus W=v^2(DM/DT)=(600^2)(4.3) but this is incorrect and I do see where I am wrong.
 
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Hi Fisicks! :smile:

You've used mdv/dt, which obviously doesn't work if m is not constant :redface:

(and dv/dt = 0, which I don't really understand)

start again, using the full version of good ol' Newton's second law …

force = rate of change of momentum :wink:
 
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