Answer:
1413.7 mi/h
Step-by-step explanation:
height in air (H) = 30,000 ft = 30,000 x 0.3048 = 9,144 m
speed in air (v) = 550 mi/h = 550 x 0.44704 = 245.872 m/s
mass of aircraft = 255,000 lb = 255,000 x 0.453592 = 115666.054 kg
magnitude of the work done by drag force (W) = 2.96 × 10^6 Btu = 2.96 × 10^6 x 1055.06 = 3,122,977,600 J
acceleration due to gravity (g) = 32.08 ft/s^{2} = 32.08 x 0.3048 = 9.8 m/s^{2}
Take note that all values above are converted to their standard units
kinetic energy in air (KE1)= 0.5m
= 0.5 x 115,666.054 x
= 3,496,182,316.8 J
potential energy in air (PE1) = mgh = 115,666.054 x 9.8 x 9,144 = 10,364,973,898.2 J
potential energy on the ground (PE2) = 0 since height (h) is 0
from the energy balance equation KE2 + PE2 = KE1 + PE1 - W
where KE2 = kinetic energy on the ground and PE2 = 0
we now have KE2 = KE1 + PE1 - W
substituting all values into the equation above we have
KE2 = 3,496,182,316.8 + 10,364,973,898.2 - 3,122,977,600
KE2 = 10738178615 J
recall that kinetic energy = 0.5m
, hence
10738178615 = 0.5 x 115666.054
=
= 185675.5
v=
v = 430.9 m/s = 430.9 x 3.28084 = 1413.7 mi/h