# Example Problem with Complete Solution

1A-1 : Kinetic and Potential Energy of an Airplane in Flight 6 pts
Gravitational acceleration is less at higher altitudes than at sea level. Assume gravitational acceleration as a function of altitude is described by g(m/s2) = 9.806 - 3.2 x 10-6 * h, where h is the altitude (relative to sea level).
Consider an aircraft flying at 750 km/h at an altitude of 12 km. Before take-off, the aircraft weighed 50 kN at sea level. Determine its:
a.) kinetic energy
b.) potential energy relative to sea level.

Read : Since gravitational acceleration is LESS at higher altitude, the gravitational potential energy of the airplane will not be quite as great as you might ordinarily expect.  We need the weight of the airplane at sea level in order to determine the mass of the airplane.  We need ot know the mass in order to calculate both the kinetic and gravitation potential energies of the plane.
Given: g(m/s2) = a - b * h v 750 km/h
a 9.8066 m/s2 h 12000 m
b 3.20E-06 s-2 Wsea level 50 kN
gc 1 kg-m/N-s2
Find: a.) Ekin ??? MJ b.) Epot ??? MJ
Assumptions: 1- Gravitational acceleration is a function of altitude only.
Equations / Data / Solve :
Let's begin by determining the mass of the airplane from the weight at sea level.
Newton's 2nd Law of Motion: Eqn 1
or Eqn 2
At sea level, according to the eqn given in the
problem statement, the acceleration of gravity is :
g 9.8066 m/s2
Now, we can solve Eqn 1 for

m and plug in values :
Eqn 3
m 5099 kg
Now, we are ready to solve the rest of the problem.
Part a.) The definition of kinetic energy is : Eqn 4
Ek 1.106E+08 J
Ek 111 MJ
Part b.) The definition of gravitational potential energy, relative to sea level, is : Eqn 5
The problem is what value of g do we use ?  Do we simply use g at the altitude of the plane? Or do we use some sort of average value of g ?