Samolot o masie 100 000 kg leci z szybkością 720 km/h na wysokości 8 km nad Ziemią. Oblicz całkowitą energię mechaniczną samolotu.
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m=100000kg
v=720km/h = 200m/s
g=10m/s
h = 8km = 8000m
Ek = 1/2 m * v^2
Ek = 0,5 * 100000kg * (200m/s)^2 = 50000kg * 40000m^2/s^2 = 200000000J = 200MJ
Ep = mgh
Ep = 100000kg * 10m/s * 8000m = 8000000000J = 8000MJ
Em = Ek+Ep = 200MJ + 8000MJ = 8200MJ
Emech = Ep + Ek
Ep = ?
m = 100 000 kg
v = 720 km/h = 720/1 * 1000m/3600s = 200 m/s
h = 8 km = 8000 m
g = 10m/s²
Ep = m * g * h
Ep = 100 000 kg * 10m/s² *8000 m
Ep = 8 000 000 000 J
Ek = m*v² / 2
Ek = 100 000 kg * (200m)² / 2
Ek = 2 000 000 000 J
Em = 10 000 000 000 J
Em = 10 000 000 kJ