An airplane (mass 80000kg) has a thrust of 160000N.
a) Estimate the work needed to reach the take-off speed of 60m/s
from rest? Neglect air drag and rolling resistance, assuming that
the acceleration is constant. You can calculate this in 2 ways:
calculate the distance and determine the energy, or use the kinetic
energy difference. Do it both ways!
b) How long is the minimum runway, assuming a safety factor of 2.
Compare this value to the shorter runway at Tallahassee Airport
(TLH).
a)
using conservation of energy
W = 0.5 m v^2 = 0.5* 80000* 60^2
W = 1.44* 10^8 J
considering the 2nd approach
we need to find the acceleration fiest
a = F/m = 160000 / 80000 = 2 m/s^2
using 3rd equation of motion
d = v^2/ ( 2 a) = 60^2 / ( 2* 2) = 900 m
then workdone stored as kE
kE = Fd = 160000* 900 = 1.44* 10^8 J
=======
b) length of runway
W = Fd
1.44* 10^8 = 160000* d
d = 900 m
for factor of safety of 2,
runway = 900* 2 = 1800 m = 1.8 km
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An airplane (mass 80000kg) has a thrust of 160000N. a) Estimate the work needed to reach...
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