Solutions - Physics
Solutions - Physics
Solutions - Physics
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dx!<br />
dt !<br />
"! # " t #<br />
i<br />
mi<br />
f xi<br />
g<br />
<br />
dx!<br />
i<br />
gt " #<br />
! dt : Integrable (3)<br />
f<br />
<strong>Physics</strong> 301: Classical Mechanics " x!<br />
i#<br />
m<br />
Problem<br />
i<br />
Set 2 Oct. 12, 2011 <br />
c) Fx " , x # ! f " x # g " x # ! m x!! : Not integrable (4)<br />
! !<br />
i<br />
i i i i i<br />
2-2. Using spherical coordinates, we can write the force applied to the particle as<br />
F! F e & F e & F e (1)<br />
r<br />
r<br />
$ $ % %<br />
But since the particle is constrained to move on the surface of a sphere, there must exist a<br />
reaction force ' e that acts on the particle. Therefore, the total force acting on the particle is<br />
F r r<br />
Ftotal ! F$ e$ & F% e % ! m!!r (2)<br />
The position vector of the particle is<br />
r ! Re (3)<br />
where R is the radius of the sphere and is constant. The acceleration of the particle is<br />
r<br />
30 CHAPTER 2<br />
r<br />
a! !! r ! R!! e<br />
(4)<br />
We must now express e!!<br />
r<br />
in terms of e<br />
r<br />
, e ! , and e " . Because the unit vectors in rectangular<br />
coordinates, e<br />
1<br />
, e2<br />
, e<br />
3<br />
, do not change with time, it is convenient to make the calculation in<br />
terms of these quantities. Using Fig. F-3, Appendix F, we see that<br />
29<br />
er<br />
$ e1 sin ! cos "% e2 sin ! sin " % e3<br />
cos ! #<br />
&<br />
e!<br />
$ e<br />
1<br />
cos ! cos "% e2 cos ! sin " ' e3<br />
sin ! &<br />
(5)<br />
&<br />
&<br />
e e sin " e cos "<br />
" $'<br />
1<br />
%<br />
2<br />
&(<br />
Then<br />
) ! !<br />
* )<br />
!<br />
!<br />
*<br />
e!<br />
$ e '" sin ! sin "% ! cos ! cos " % e ! cos ! sin "% " sin ! cos " ' e ! ! sin !<br />
r<br />
1 2<br />
$ e ! " sin ! % e ! !<br />
" !<br />
3<br />
(6)<br />
Similarly,<br />
e! $' e ! ! % e ! " cos ! (7)<br />
! r "<br />
e! $' e ! " sin ! ' e ! " cos ! (8)<br />
" r<br />
!<br />
And, further,<br />
)<br />
! 2 2 2 2<br />
" sin ! ! ! * )!! ! ! " sin ! cos ! * ) 2 ! !"!<br />
cos ! " sin ! *<br />
!! e $' e % % e ' % e % !! (9)<br />
r r ! "<br />
which is the only second time derivative needed.<br />
The total force acting on the particle is<br />
and the components are<br />
F<br />
!<br />
F<br />
"<br />
F $ mr!! $ mR!!e (10)<br />
total<br />
$ mR '<br />
)!! ! ! " 2 sin ! cos ! *<br />
) 2! !"! cos ! !! " sin !*<br />
$ mR %<br />
r<br />
(11)
which 2-4. gives One of the the correct balls’ result, 2<br />
height as can in be (4) described for the limit by k y, % y0.<br />
' v t & gt . The amount of time it<br />
0 0<br />
2<br />
takes to rise and fall to its initial height is therefore given by 2v0<br />
g . If the time it takes to cycle<br />
2-10. the ball through The differential the juggler’s equation hands we is are ( % asked 0.9 s , to then solve there is Equation must be 3 (2.22), balls which in the air is x"" during $% k"x<br />
. that<br />
Using time (. the A single given ball values, must the stay plots in are the shown air for at in least the figure. 3(, so the Of course, condition the is reader 2v0<br />
g will ) 3(<br />
not , or be able<br />
to distinguish & 1between the results shown here and the analytical results. The reader will have to<br />
v 0<br />
) 13.2 m * s .<br />
take the word of the author that the graphs were obtained using numerical methods on a<br />
%8<br />
computer. 2-5. The results obtained were at most within 10 of the analytical solution.<br />
flightpath v vs t<br />
10<br />
v (m/s)<br />
5<br />
N<br />
e r<br />
0 5 10 15 20 25 30<br />
plane<br />
mg<br />
t (s)<br />
point of maximum<br />
accelerationx vs t<br />
a) From the force diagram we have & m %! mv 2 R"<br />
2<br />
m% '! mv R"<br />
50<br />
r<br />
N g e . The acceleration that the pilot feels is<br />
N g e , which has a maximum magnitude at the bottom of the maneuver.<br />
b) If the acceleration felt by the pilot must be less than 9g, then we have<br />
& 1<br />
! 3* 330 mt *(s)<br />
s "<br />
2<br />
v<br />
R ) %<br />
8g<br />
8* 9.8 m * s<br />
A circle smaller than this will result in pilot blackout.<br />
2-6.<br />
x (m)<br />
v (m/s)<br />
100<br />
0<br />
0 5 10 15 20 25 30<br />
10<br />
5<br />
v vs x<br />
& 2<br />
0<br />
0 20 40 60 80<br />
x (m)<br />
r<br />
! 12.5 km<br />
(1)<br />
100<br />
2-11. The equation of motion is<br />
2<br />
Let the origin of our coordinate system be<br />
dx<br />
at the tail<br />
2<br />
m $% kmv end # mgof the cattle (or the closest cow/bull). (1)<br />
2<br />
dt<br />
a) The bales are moving initially at the speed of the plane when dropped. Describe one of<br />
This NEWTONIAN<br />
these<br />
equation MECHANICS—SINGLE<br />
bales by<br />
can<br />
the parametric<br />
be solved exactly PARTICLE<br />
equations<br />
in the same way as in problem 2-12 and we find 37<br />
x% x0 ' v0t<br />
(1)<br />
2<br />
1 ! g#<br />
kv "<br />
log<br />
0<br />
x $ % 2 &<br />
(2)<br />
2k ' g#<br />
kv (<br />
where the origin is taken to be the point at which v $ v0<br />
so that the initial condition is<br />
xv ) $ v 0 * $ 0 . Thus, the distance from the point v $ v0<br />
to the point v $ v1<br />
is<br />
2<br />
1 ! g#<br />
kv "<br />
0<br />
sv ) 0<br />
+ v1*<br />
$ log % 2 &<br />
2k ' g#<br />
kv1<br />
(<br />
(3)<br />
2-12. The equation of motion for the upward motion is<br />
Using the relation<br />
we can rewrite (1) as<br />
2<br />
dx<br />
2<br />
$# mkv # mg (1)<br />
2<br />
m<br />
dt<br />
2<br />
d x dv dv dx dv<br />
v<br />
2<br />
dt dt dx dt dx<br />
$ $ $ (2)
d<br />
max<br />
2<br />
v0<br />
%<br />
g $<br />
" 1'<br />
sin #<br />
2-15.<br />
mg sin θ<br />
mg<br />
θ<br />
The equation of motion along the plane is<br />
Rewriting this equation in the form<br />
dv<br />
m mg km<br />
dt<br />
2<br />
% sin 6 & v (1)<br />
1 dv<br />
% dt<br />
(2)<br />
42 k g<br />
2<br />
CHAPTER 2<br />
sin 6 & v<br />
k<br />
We know that the velocity of the particle continues to increase with time (i.e., dv dt ! 0 ), so that<br />
2<br />
" g k# sin v<br />
find<br />
$ ! . Therefore, we must use Eq. (E.5a), Appendix E, to perform the integration. We<br />
1 1<br />
v<br />
tanh<br />
k g * g +<br />
sin $ * sin $ +<br />
k<br />
, k -<br />
% 1 & ' ( )<br />
The initial condition v(t = 0) = 0 implies C = 0. Therefore,<br />
" gk #<br />
g<br />
v ( sin $ tanh sin $ t<br />
k<br />
t<br />
C<br />
(3)<br />
( dx<br />
dt<br />
(4)<br />
We can integrate this equation to obtain the displacement x as a function of time:<br />
Using Eq. (E.17a), Appendix E, we obtain<br />
" gk #<br />
g<br />
x( sin $ tanh sin $<br />
k<br />
. t dt<br />
x (<br />
" gk sin $ t#<br />
g ln cosh<br />
sin $<br />
k<br />
gk sin $<br />
) C/ (5)<br />
The initial condition x(t = 0) = 0 implies C/ = 0. Therefore, the relation between d and t is<br />
From this equation, we can easily find<br />
" gk $ t#<br />
1 d ( ln cosh sin<br />
(6)<br />
k<br />
" e dk<br />
#<br />
% 1<br />
cosh<br />
t ( (7)<br />
gk sin $<br />
2-16. The only force which is applied to the article is the component of the gravitational force<br />
along the slope: mg sin 0. So the acceleration is g sin 0. Therefore the velocity and displacement<br />
along the slope for upward motion are described by:<br />
" 0#<br />
where the initial conditions vt " ( 0# ( v0<br />
and " 0#<br />
v( v0 % g sin t<br />
(1)<br />
1<br />
2<br />
x( v0t % " g sin 0 # t<br />
(2)<br />
2<br />
xt( ( 0 have been used.<br />
At the highest position the velocity becomes zero, so the time required to reach the highest
" #"<br />
2<br />
2!gs VB<br />
VB<br />
#<br />
2!<br />
gs<br />
V # 15.6 m/sec<br />
B<br />
2-25.<br />
a) At A, the forces on the ball are:<br />
N<br />
The track counters the gravitational force and provides centripetal acceleration<br />
Get v by conservation of energy:<br />
So<br />
b) At B the forces are:<br />
mg<br />
2<br />
N" mg # mv R<br />
E # T $ U # 0 $ mgh<br />
top top top<br />
1<br />
E T U mv<br />
2<br />
2<br />
A<br />
#<br />
A<br />
$<br />
A<br />
# $<br />
E # E % v # 2gh<br />
top<br />
A<br />
N # mg $ m2gh R<br />
& 2h'<br />
N # mg( 1 $<br />
*<br />
)<br />
R +<br />
0<br />
N<br />
45˚<br />
mg<br />
2<br />
N mv R mg<br />
Get v by conservation of energy. From a), Etotal<br />
1 2<br />
At B, E# m v $ mgh-<br />
2<br />
# $ cos 45,<br />
2<br />
# mv R $ mg 2<br />
(1)<br />
# mgh .
R 2<br />
R<br />
R 45˚<br />
Rcos 45˚ = R 2<br />
h′<br />
So<br />
Etotal ! TB " UB<br />
Solving for<br />
2<br />
v<br />
becomes:<br />
R<br />
1<br />
R ! " h# or h# ! R $ ' 1 &<br />
%<br />
2<br />
)<br />
(<br />
2 *<br />
mgh mgR $ 1 % 1<br />
! ' 1 & "<br />
)<br />
(<br />
2 * 2<br />
mv<br />
2<br />
Substituting into (1):<br />
1<br />
2 + $ %<br />
- gh & gR' 1& (<br />
, ! v<br />
) 2 * .<br />
/ 0<br />
2<br />
2h<br />
3<br />
N mg + $ %<br />
! - "' & 2(<br />
,<br />
R ) 2 *.<br />
/ 0<br />
c) From b)<br />
B<br />
! 2 + h & R " R 2,<br />
/ 0<br />
2<br />
v g<br />
d) This is a projectile motion problem<br />
1 2 12<br />
v! + 2g h & R " R 2 ,<br />
/ 0<br />
45˚<br />
B<br />
45˚<br />
Put the origin at A.<br />
The equations:<br />
become<br />
Solve (3) for t when y = 0 (ball lands).<br />
A<br />
x! x " v t<br />
0 x0<br />
1<br />
y! y0 " vy0t & gt<br />
2<br />
2<br />
R v<br />
x ! " B<br />
t (2)<br />
2 2<br />
v B<br />
1 2<br />
# (3)<br />
y! h " t & gt<br />
2 2
2<br />
gt ! 2 vBt ! 2h#<br />
" 0<br />
t "<br />
2<br />
2<br />
B<br />
2<br />
B<br />
8<br />
v $ v % gh#<br />
2g<br />
We discard the negative root since it gives a negative time. Substituting into (2):<br />
2<br />
NEWTONIAN MECHANICS—SINGLE PARTICLE R v &<br />
B<br />
2 vB<br />
$ 2vB<br />
% 8gh#<br />
'<br />
71<br />
x " % ( )<br />
2 2 ( 2g<br />
*<br />
)<br />
+<br />
The equilibrium point (where dU d! " 0 ) that we wish to look at is clearly ! = 0. At that point,<br />
Using the previous expressions for v B<br />
and h# yields<br />
we have dU 2 d! 2 " mg # R % b 2$<br />
, which is stable for R&<br />
b 2 and unstable for R' b (2 . We can<br />
12<br />
use the results of Problem 2-46 & 2 3 2 2 '<br />
x" to obtain<br />
, 2 ! 1-R<br />
stability<br />
% h %<br />
(<br />
h<br />
for<br />
!<br />
the<br />
R<br />
case<br />
% 2<br />
R<br />
R<br />
" b 2 , where we will find that<br />
* 2 )<br />
the first non-trivial result is in fourth order and is negative. We therefore + have an equilibrium at<br />
! = 0 which is stable for R& b 2 and unstable for R) b 2 .<br />
e) Ux ( )" mgy( x)<br />
, with y(0)<br />
" h, so U( x ) has the shape of the track.<br />
<br />
3 2<br />
2-43. F "% kx + kx *<br />
2-26. All of the kinetic energy of the block goes into compressing the spring, so that<br />
2 2<br />
mv 2" kx 2, or x" v m k ! 23 . m , where x is the maximum<br />
4<br />
compression and the given<br />
values have been substituted. When U # x 1 2 1 x<br />
$ "%<br />
there , is F dx "<br />
2<br />
a rough 2 kx %<br />
floor, 4<br />
k it * exerts a force / mg k<br />
in a direction<br />
that opposes the block’s velocity. It therefore does an amount of work 1 / mgd k<br />
in slowing the<br />
2<br />
To sketch U(x), we note that for small x, U(x) behaves like the parabola kx . For large x, the<br />
block down after traveling across the floor a distance d. After 2 m of floor, 2 the block has energy<br />
mv<br />
2 2 ! /<br />
kmgd<br />
, which now goes into<br />
4<br />
1 x compressing the spring and still overcoming the friction<br />
behavior is determined by % k<br />
2<br />
on the floor, which is kx % 4/<br />
mgx * . Use of the quadratic formula gives<br />
2 2<br />
k<br />
U(x)<br />
2 2<br />
/ mg 0/ mg1<br />
mv 2/<br />
mgd<br />
x "! % 2 3 % !<br />
(1)<br />
k 4 k 5 k k<br />
E 0<br />
Upon substitution of the given values, the result is ! 1.12 m.<br />
E 1<br />
E 2<br />
2-27.<br />
x 4<br />
x 5<br />
x<br />
x 1 x 2<br />
x 3 E 3<br />
= 0<br />
0.6 m<br />
E 4<br />
1 2<br />
To lift a small mass dm of rope onto the table, E" mv an amount + U # x$<br />
2<br />
of work dW " , dm- g , z0<br />
! z-<br />
must be<br />
done on it, where z<br />
0<br />
" 06 . m is the height of the table. The total amount of work that needs to be<br />
For E " E 0<br />
, the motion is unbounded; the particle may be anywhere.<br />
done is the integration over all the small segments of rope, giving<br />
For E " E 1<br />
(at the maxima in U(x)) the particle is at a point of unstable equilibrium. It may<br />
2<br />
z0<br />
( ) ( ) / gz<br />
remain at rest where it is, but if perturbed<br />
0<br />
W " 6<br />
slightly, / dz g z it<br />
0<br />
! will z " move away from the equilibrium. (1)<br />
0 2<br />
dU<br />
When What is we the substitute value of E/ 1" mL We find ", 04 . the kgx -<br />
values , 4 m-<br />
, by we setting obtain W ! 0<br />
dx " . 18 . J .<br />
x = 0, - * are the equilibrium points<br />
3 2<br />
0 " kx % kx *<br />
1 2 1 2 1<br />
U# -* $ " E1<br />
" k* % k*<br />
" k*<br />
2<br />
2 4 4<br />
For E " E 2<br />
, the particle is either bounded and oscillates between % x2<br />
and x 2<br />
; or the particle<br />
comes in from -. to - and returns to -..<br />
x 3
m<br />
1<br />
% m2<br />
m1 % m2<br />
At equilibrium, like in previous problem, we have<br />
72 CHAPTER 2<br />
2 2<br />
32<br />
Gm1m2 m1v1 Gm2 2 r1<br />
2 d<br />
# $ v1<br />
# $ " # ! #<br />
!<br />
2<br />
For E , the particle d is either r at the stable d( mequilibrium % m ) point v x = 0, Gm or ( beyond % m ) x!"<br />
x .<br />
3<br />
! 0<br />
1 1 2 1 1 2<br />
4<br />
The For E result , the will particle be the<br />
4<br />
comes same in if from we consider "# to " the x5<br />
and equilibrium returns. of forces acting on 2nd star.<br />
76 CHAPTER 2<br />
2-44. 2-50.<br />
So one can see that in this problem x = a and x = –a are unstable equilibrium positions, and x = 0<br />
is a stable t<br />
d &<br />
equilibrium mv<br />
0 '<br />
position.<br />
& mv<br />
0 ' mv<br />
0 T θ T Ft<br />
a)<br />
# F$ d # # Ft $ v()<br />
t #<br />
dt ( 2 2 T 2<br />
v ) - (<br />
0 v )<br />
2 2<br />
v<br />
2 F t<br />
( 1* ) (<br />
4Ux<br />
0<br />
1* )<br />
k 4U0<br />
c) Around the 1 *<br />
m<br />
2 origin, F<br />
2 2<br />
0<br />
%<br />
2<br />
+ c , "# kx<br />
+ 2c , m 1 c m 2<br />
a<br />
$ # % ! & m<br />
& 2 ma c<br />
d) To escape to infinity from x = 0, the t m 1 particle g 2 m 2 g 2 2<br />
c & needs to<br />
2 Fget t at least ' to the peak of the potential,<br />
$ xt ()#-<br />
v( t)<br />
dt # ( m0 % * m<br />
2<br />
2 0)<br />
From the figure, the forces acting mv on the 0 masses Fgive + the equations c , of motion<br />
min<br />
2U<br />
0<br />
& Umax & U0 % vmin<br />
&<br />
2 m1 !! x1<br />
! m1g<br />
$ T m<br />
b)<br />
(1)<br />
e) From energy conservation, we v have m x !! m g T %<br />
(2)<br />
2 2 !<br />
2<br />
$ 2 cos<br />
2 2 2<br />
2<br />
where x2<br />
is related to x1<br />
by mvthe Ux<br />
relation 0<br />
mvmin<br />
dx 2U<br />
0<br />
' x (<br />
) & % & v &<br />
2 * 1 #<br />
2<br />
2 a 2 dt m ,<br />
+<br />
a -<br />
We note that, in the ideal case, because & b$<br />
x ' 2<br />
1 2<br />
xthe 2<br />
! initial velocity $ d is the escape velocity found in d), (3)<br />
ideally x is always smaller or equal to a, then from 4 the above expression,<br />
cos ) 1<br />
2* + . At equilibrium, !! x1 ! x!! 2 ! 0 and T ! ' mt<br />
1<br />
g . This 8Ugives as the equilibrium<br />
0<br />
x<br />
a exp ' (<br />
2<br />
* t<br />
( 2 + # 1<br />
values c) From for the a) we coordinates find m dx ma a ) x<br />
*<br />
, , ma - +<br />
-<br />
t& ln ( t)<br />
2<br />
2U . & % x &<br />
0 '<br />
0<br />
x ( 8U0<br />
a<br />
vm<br />
# x4<br />
md ' '<br />
1<br />
8U<br />
( (<br />
0 1<br />
0<br />
* #<br />
,<br />
2 + x10<br />
t! # b$<br />
exp t 1<br />
(4)<br />
4m1 $ m<br />
2 2<br />
a - * )<br />
2<br />
v<br />
,<br />
*<br />
,<br />
+<br />
ma - +<br />
-<br />
2<br />
F 1 *<br />
2<br />
x<br />
c<br />
md<br />
2<br />
x20<br />
!<br />
(5)<br />
NEWTONIAN F<br />
2<br />
Now if 10<br />
4m1 $ m<br />
2 2<br />
m # MECHANICS—SINGLE , then<br />
PARTICLE 75<br />
0<br />
We recognize that our expression x 10<br />
is identical to Equation (2.105), and has the same<br />
requirement that m2 m<br />
1<br />
, 2 for<br />
c<br />
when v!<br />
c 2 , we have t ! the ! 0.55 equilibrium year to exist. When the system is in motion, the<br />
descriptive equations are obtained<br />
10 3<br />
from the force laws:<br />
99c<br />
t<br />
when v = 99% c, we have t ! ! 6.67 years m2&<br />
b$<br />
x1'<br />
10 199 m1( !! x1<br />
$ g) ! ( x!! 2 $ g)<br />
(6)<br />
4x2<br />
2-53.<br />
To examine stability, let us expand the coordinates about their equilibrium values and look at<br />
their 2-51. F is a behavior conservative for small force displacements. when there exists Let a - non-singular<br />
1<br />
. x1 $ x10<br />
and potential -<br />
2<br />
. x2 $ function x2<br />
0<br />
. In the U(x) calculations, satisfying<br />
F(x) = –grad(U(x)). So if F is conservative, its components satisfy the following relations<br />
take terms dv in -<br />
1<br />
and -<br />
2<br />
, and their time derivatives, only up to first order. Equation (3) then<br />
2 dv b<br />
mv0<br />
a) m !" bv # ! " dt # v()<br />
t !<br />
2<br />
becomes dt-2 " $ (m1 m% 2v )-<br />
1<br />
. When %<br />
m written in btv terms / F of these new coordinates, the equation of<br />
0<br />
$ m/<br />
F<br />
x y<br />
&<br />
motion becomes<br />
/ y / x<br />
999m<br />
Now let v(t) = v 0<br />
/1000 , one finds t ! ! 138.7 hours<br />
2 2<br />
32<br />
and so on.<br />
.<br />
vb<br />
0<br />
g&<br />
4m1 $ m2<br />
!!<br />
'<br />
- !$<br />
1<br />
1<br />
4mm m / m d -<br />
(7)<br />
a) In this case all relations above are satisfied, so F is indeed a conservative force.<br />
and % ! d (& b$<br />
x '<br />
b)<br />
t<br />
m & btv0<br />
$ m'<br />
! vdt ! ( )<br />
%<br />
x() t<br />
ln<br />
b * m +<br />
0<br />
v<br />
&<br />
1 2 1 2<br />
2<br />
/ U<br />
bx<br />
F ( , )<br />
x<br />
&# & ayz ) bx ) c % U &# ayzx # # cx ) f1 y z<br />
(1)<br />
/ x<br />
2<br />
where f ( y, z)<br />
1<br />
is a function of only y and z<br />
/ U<br />
F ( , )<br />
y<br />
&# & axz ) bz % U & # ayzx # byz ) f<br />
2 x z<br />
(2)<br />
/ y<br />
We use the value of t found in question a) to find the corresponding distance<br />
'<br />
t
NEWTONIAN MECHANICS—SINGLE PARTICLE 77<br />
where<br />
f ( x, z)<br />
2<br />
is a function of only x and z<br />
! U<br />
F axy by c U ayzx byz f ( , )<br />
z<br />
"% " # # $ "% % #<br />
3 y z<br />
(3)<br />
! z<br />
then from (1), (2), (3) we find that<br />
where C is a arbitrary constant.<br />
bx<br />
2<br />
2<br />
2<br />
U "% axyz % byz % cx % # C<br />
b) Using the same method we find that F in this case is a conservative force, and its potential<br />
is<br />
U " % zexp( % x) % yln<br />
z # C<br />
c) Using the same method we find that F in this case is a conservative force, and its potential<br />
is ( using the result of problem 1-31b):<br />
U " % aln<br />
r<br />
2-54.<br />
a) Terminal velocity means final steady velocity (here we assume that the potato reaches this<br />
velocity before the impact with the Earth) when the total force acting on the potato is zero.<br />
b)<br />
mg = kmv and consequently v" g k " 1000 m/s .<br />
dv F dx dv vdv<br />
" " %( g# kv)<br />
$ " dt " % $ dx " % $<br />
dt m v g # kv<br />
& &<br />
g # kv<br />
x<br />
0<br />
0<br />
v0<br />
x<br />
v g g<br />
" # ln " 679.7 m<br />
k k g # kv<br />
0<br />
max 2<br />
0<br />
where v is the initial velocity of the potato.<br />
0<br />
2-55. Let’s denote vx0<br />
and v<br />
y0<br />
the initial horizontal and vertical velocity of the pumpkin.<br />
Evidently, vx0<br />
" v y 0<br />
in this problem.<br />
dvx<br />
dx dv vx0<br />
% vxf<br />
m " F "% mkv $ % " % dt " $ x " (1)<br />
dt v kv k<br />
x<br />
x x f<br />
x<br />
x<br />
where the suffix f always denote the final value. From the second equality of (1), we have<br />
Combining (1) and (2) we have<br />
dv<br />
% " $ " (2)<br />
x<br />
% kt<br />
dt v<br />
f<br />
xf<br />
vx0e<br />
kvx<br />
x<br />
f<br />
v<br />
k<br />
x0<br />
% kt<br />
" ' 1 %<br />
f<br />
(<br />
e (3)