Solutions to Problems on Potential Energy and Orbits, Exercises of Classical and Relativistic Mechanics

Solutions to problems related to the potential energy of a particle and the shapes of its orbits. The solutions involve calculating the graph of the potential energy function, determining the particle's behavior based on its energy, and finding the relationship between the particle's energy and the shape of its orbit.

Typology: Exercises

2011/2012

Uploaded on 07/19/2012

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5. Sketch the graph of Veff(r) when V=k
rand describe what a particle in this potential
would do, depending on it’s energy E.
Solution: We have Veff(r) = j2
2mr2k
r=k j2
2mk r
r2!. This is minimized when r=j2
mk , and
then Veff =k2m
2j2. Since 1
2m˙r2must be nonnegative, we know that a particles total energy can
never be less than k2m
2j2. If a particles total energy is positive, then rcan go to infinity. If E < 0,
then the particle will be stay in between to values of r, determined by when the energy equals Veff .
6. Show θ=θ0+ arccos
j
mr k
j
q2E
m+k2
j2
.
Solution: Z(j/mr2)dr
q2
m(EVeff (r))
=Z(j/mr2)dr
q2
m(E+k
rj2
2mr2)
=Zdw
q2Em
j2+2km
j2ww2
, where
w=1
r. Using the fact Zdx
ax2+bx +c=1
aarccos 2ax b
b24acwhen a < 0, we have
Zdw
q2Em
j2+2km
j2w1
jw2
= arccos
2w2km
j2
q4k2m2
j4+ 42Em
j2
= arccos
j
mr k
j
qk2
j2+2E
m
. So θ=θ0+
arccos
j
mr k
j
q2E
m+k2
j2
.
2
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  1. Sketch the graph of Veff (r) when V = − kr and describe what a particle in this potential would do, depending on it’s energy E.

Solution: We have Veff (r) = (^2) mrj^22 − kr = k

( (^) j 2 2 mkr 2 −^ r

. This is minimized when r = (^) mkj^2 , and

then Veff = − k 22 jm 2. Since^12 m r˙^2 must be nonnegative, we know that a particles total energy can never be less than − k 22 jm 2. If a particles total energy is positive, then r can go to infinity. If E < 0, then the particle will be stay in between to values of r, determined by when the energy equals Veff.

  1. Show θ = θ 0 + arccos mr^ j −^ kj √ (^2) E m +^ k j^22

Solution:

∫ (^) (j/mr (^2) )dr √ (^2) m (E^ −^ Veff^ (r))

∫ (^) (j/mr (^2) )dr √ (^2) m (E^ +^ kr −^2 mrj^22 )

∫ (^) dw √ (^2) Em j^2 +^2 kmj^2 w^ −^ w^2

, where

w = (^1) r. Using the fact

∫ (^) dx √ax (^2) + bx + c = − √^1 −a arccos

( (^) − 2 ax − b √b (^2) − 4 ac

when a < 0, we have

∫ (^) dw √ (^2) Em j^2 +^2 kmj^2 w^ −^1 j w^2

= arccos

 (^) √ (^42) kw (^2) m^ − 2 2 kmj^2 j^4 + 4^2 Emj^2

 (^) = arccos

 √mr jk 2 −^ kj j^2 +^2 mE

. So θ = θ 0 +

arccos mr^ j −^ kj √ (^2) E m +^ k j^22

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  1. Letting p = (^) kmj^2 and e =

1 +^2 mkEj 22 , show θ = θ 0 + arccos

( (^) p/r − 1 e

Solution: θ = θ 0 + arccos mr^ j −^ kj √ (^2) E m +^ k j^22

= θ 0 + arccos mr^ j −^ kj jk^ √^2 mkEj 22 + 1=^ θ^0 + arccos √mr^ j jk^ −^1 (^2) mkEj 22 + 1= θ 0 + arccos

( (^) p/r − 1 e

. Solving for r gives r = (^) 1 + e cos(pθ − θ 0 ).

  1. The equation r = (^) 1 + e cos(pθ − θ 0 ) describes an ellipse, parabola or hyperbola based on the value of e. Solution: By a rotation, we can assume θ 0 = 0. So we have p = r +er cos θ or p = √x^2 + y^2 +ex. So x^2 + y^2 = p^2 − 2 epx + x^2 , or (1 − e^2 )x^2 + 2epx + y^2 = p^2. If e = 0, we have p^2 = x^2 + y^2 , the equation of a circle. If 0 < e < 1, let k = (^1) −ep e 2. Then we have x^2 + 2kx + (^1) −y^2 e 2 = (^1) −p^2 e 2 = (x − k)^2 + (^1) −y^2 e 2 = p^2 1 − e^2 +^ k^2 , and ellipse. If e = 1, we have 2px = −y^2 + p^2 , a parabola. If e > 1, let k = (^1) −ep e 2. Then we have x^2 + 2kx + (^1) −y^2 e 2 = (^1) −p^2 e 2 = (x − k)^2 − (^) e 2 y (^) −^2 1 = p^2 1 − e^2 +^ k^2 , a hyperbola.
  2. How are the 3 kinds of orbits related to energy? Solution: The hyperbola corresponds to e > 1, which requires the energy to be positive. The parabola correspond to e = 1, which requires energy to be 0. The ellipse corresponds to 0 < e < 1 which corresponds which requires energy to be negative.

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