p11 099

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99. First, we convert the angular velocity: ω = (2000)(2π/60) = 209 rad/s. Also, we convert the plane’s

speed to SI units: (480)(1000/3600) = 133 m/s. We use Eq. 11-18 in part (a) and (implicitly) Eq. 4-39
in part (b).

(a) The speed of the tip as seen by the pilot is

v

t

= ωr = (209 rad/s)(1.5 m) = 314 m/s

which (since the radius is given to only two significant figures) we write as v = 3.1

× 10

2

m/s.

(b) The plane’s velocity 

v

p

and the velocity of the tip 

v

t

(found in the plane’s frame of reference), in

any of the tip’s positions, must be perpendicular to each other. Thus, the speed as seen by an
observer on the ground is

v =



v

2

p

+ v

2

t

=



(133 m/s)

2

+ (314 m/s)

2

= 3.4

× 10

2

m/s .


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