At the equator, the radius of the Earth is approximately 6370 km. A plane flies at a very low altitude at a constant speed of v = 288 m/s. Upon landing, the plane can produce an average deceleration of a = 19 m/s2. 1. How long will it take the plane, in seconds, to circle the Earth at the equator? 2. What is the numeric value for the minimum landing distance, d (in meters), this plane needs to come to rest?
We all know the relationship between velocity-distance-time \[v=\frac{ x }{ t }\]
So if we substitute with distance x=6,370 km=6,370,000 m and velocity v=288 m/s we can get the time to circle the earth at the equator \[t=\frac{ x }{ v }=\frac{ 6370000 }{ 288 }=22118\] seconds
For the second part:
wait, it says it's wrong. I think we have to square the distance since 6370 is radius, right?
We know the law of motion that states : \[v_{f}^{2}=v_{0}^{2}-2*a*d\] where a is the deceleration and d is the minimum distance to stop completely
so \[288^{2}=0^2-2*19*d\] therefore \[d=2182\] m
wait, it says the answer for the first part is wrong
I see Thank you. I will correct it now. Good to see others like you revise what you write
For the first part, we would calculate the perimeter of the earth that the plane will circle it. Earth perimeter/circumference = \[\pi(r)^2=\pi(6,370,000)^2=1.275274\times 10^{14}\] meter
then the time required to circle the earth at the equator is \[t=\frac{ x }{ v }=\frac{ 1.275274\times 10^{14}/288}\] =\[4.428\times 10^{11}\] seconds
Hope that helps you.
Join our real-time social learning platform and learn together with your friends!