An airplane flies due west at 120 km/h. At the same
time, the wind blows it due north at 40.0 km/h. What is the plane's
resultant velocity?
Use Trigonometry on solving the problem.
Here the earth is one reference frame(S) and the air is the other reference frame(S') moving with respect to the first.
Then, u=40 km/h is the velocity of the air with respect to the ground,v'=120 km/h is the velocity of the plane with respect to the air and v is the velocity of the plane with respect to the ground.
The angle a is the angle N of W of the plane's course with respect to the ground and is given by
tan(a)=u/v'=40/120=1/3.
Therefore, a=tan-1(1/3)=18.40.
The airplane's speed with respect to the ground is given by v=squareroot(v'2+u2)=squareroot(1202+402)=126.5 km/h.
This is the plane's resultant velocity ie. both its magnitude and the angle it makes with the westward direction.
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