Engineering, 24.11.2020 18:40 mutesheep
An aircraft has the following short period approximation:
α/δ e= (-0.746s-208.6)/(675s^2+ 1361.6s+5452.45)
Find the natural frequency, damping ratio, and the steady-state value of AOA in response to a unit step input using the final value theorem.
Answers: 3
Engineering, 04.07.2019 18:10
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Answers: 1
Engineering, 04.07.2019 18:10
Water in a partially filled large tank is to be supplied to the roof top, which is 8 m above the water level in the tank, through a 2.2-cm-internal-diameter pipe by maintaining a constant air pressure of 300 kpa (gage) in the tank. if the head loss in the piping is 2 m of water, determine the discharge rate of the supply of water to the roof top in liters per second.
Answers: 3
Engineering, 04.07.2019 19:10
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Answers: 3
An aircraft has the following short period approximation:
α/δ e= (-0.746s-208.6)/(675s^2+ 1361.6s...
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