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3.92:<br />

The x-position of the plane is<br />

( 236 m/s) t and the x-position of the rocket is<br />

2<br />

2<br />

(236 m/s) t + 1/ 2(3.00)(9.80 m/s )cos30°(<br />

t − T ) . The graphs of these two have the form,<br />

If we take y = 0 to be the altitude of the airliner, then<br />

y( t)<br />

T<br />

graph looks like<br />

2<br />

2<br />

2<br />

= −1/<br />

2gT<br />

− gT ( t − T ) + 1/ 2(3.00)(9.80 m/s )(sin 30°<br />

)( t − ) for the rocket. This<br />

By setting y = 0 for the rocket, we can solve for t in terms of<br />

2 2<br />

2<br />

2<br />

2<br />

T,<br />

0 = −(4.90 m/s ) T − (9.80 m/s ) T(<br />

t − T ) + (7.35 m/s )( t − T)<br />

. Using the quadratic<br />

formula for the variable x = t − T, we find<br />

2<br />

(9.80 m/s ) T +<br />

2 2<br />

2 2<br />

(9.80 m/s T ) + (4)(7.35 m/s )(4.9) T<br />

x = t − T =<br />

or t = 2.72T.<br />

Now, using<br />

2<br />

2(7.35 m/s )<br />

the condition that x − x 1000 m,<br />

we find<br />

rocket plane<br />

=<br />

2<br />

2<br />

2<br />

(236 m/s) t + (12.7 m/s ) × ( t − T ) − (236 m/s) t = 1000 m, or (1.72T<br />

)<br />

2 = 78.6 s .<br />

Therefore T = 5.15s.<br />

3.93: a) Taking all units to be in km and h, we have three equations. We know that<br />

heading upstream v<br />

c / w<br />

− vw<br />

/ G<br />

= 2 where v<br />

c / w<br />

is the speed of the curve relative to water<br />

and v<br />

w / G<br />

is the speed of the water relative to the ground. We know that heading<br />

downstream for a time t, ( vc / w<br />

+ vw<br />

/ G<br />

) t = 5.<br />

We also know that for the bottle<br />

v w / G<br />

( t + 1) = 3. Solving these three equations for vw / G<br />

= x, vc<br />

/ w<br />

= 2 + x, therefore<br />

3<br />

( 2 + x + x)<br />

t = 5 or ( 2 + 2x ) t = 5.<br />

Also t = 3/<br />

x −1,<br />

so ( 2 2x )( −1)<br />

= 5 or<br />

+<br />

x<br />

2x 2 + x − 6 = 0. The positive solution is x = v w / G<br />

= 1.5 km/h.<br />

b) v 2 km/h + v 3.5 km/h.<br />

c / w<br />

=<br />

w/G<br />

=

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