Dynamics 2e 393
Problem 2.299
A plane is initially flying north with a speed
v0D430 mph
relative to the ground
while the wind has a constant speed
vWD12 mph
in the north-south direction.
The plane performs a circular turn with radius of
⇢D0:45 mi
. Assume that the
airspeed indicator on the plane measures the absolute value of the component
of the relative velocity of the plane with respect to the air in the direction of
motion. Then determine the value of the tangential component of the airplane’s
acceleration when the airplane is halfway through the turn, assuming that the
airplane maintains constant the reading of the airspeed indicator.
Solution
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