Calculate the Coriolis acceleration of an aeroplane flying along the equator due east at a speed of 300m/s⁻¹. Please explain
Angular speed of the Earth:
ω=2πf=24∗3600s6.28=7.27∗10−5s−1
Coriolis acceleration:
aC=2[ω×v]=2ωvaC=2∗7.27∗10−5s−1∗300m/s=0.044m/s2
Answer: aC=0.044m/s2