Department of Physics, Portland State University
Ph 425 (Classical Mechanics II) : Mid-Term Test (open-book exam)
2:00 3:30 pm, 26 April 2000 Dr. R. Egerton
Answers should indicate how the results are obtained, with explanatory words as necessary.
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G = 6.67 x 10-11 N m2/kg2 e 0 = 8.85 x 10-12 F/m e = 1.60 x 10-19 C
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1. A hole is drilled at the south pole, towards the center of the earth (mass M) to a depth of one half the earths radius Re. A rock (mass m) is dropped into the hole from rest. Derive expressions for:
2. (a) A planet is held in a circular orbit (radius a) by a central force:
F(r) = k/r2 c/r4 . Find the minimum value of a for which the orbit is stable.
(b) Give one reason why the laws of mechanics were developed on a planet whose orbit has a low eccentricity.
3. (a) A mass m makes a direct collision (coefficient of restitution e ) with a stationary mass M and a fraction a of its kinetic energy is liberated as heat. What is the ratio m/M ?
(b) For what kind of direct collision could m/M not be calculated, knowing of a and e ?
4. Two uniform solid spheres, each of radius r and mass m, are joined by a thin rod of length L and mass M which is aligned along the line joining the centers of the spheres. Specify:
(a) the center of mass of the object, measured relative to the center of the rod;
5. 100keV alpha-particles are elastically scattered through 60° by gold nuclei (Z=79). Calculate: (a) the impact parameter of these 60° collisions;
(b) the differential cross section for scattering at this angle.
Ph 425 Mid-Term Answers (R. Egerton)
(b) Since F(r) is proportional to r, weight = mg (r/re) = mg/2
(c) Gain in gravitational PE = work done on rock = ò F(r)dr
= - ò GmMr/re3dr = - GmM[re2- re2/4] / re3 = - (3/4) GmM/re
Increase in gravitational potential = PE/m = - (3/4) GM/re
(d) K = loss of gravitational PE = (3/4) GmM/re
(e) Impulse P = change in momentum of rock = mv - 0 = (2mK)1/2
= m(1.5GM/re)1/2
(f) Momentum of system before stone is released = M.0 + m.0 = 0
= momentum of system after = M.v' + m v' , therefore v = 0.
f(a) + (a/3) f (a) < 0 , giving:
- k/a2 c/a4 + (a/3) [ 2k/a3 + 4c/a5 ] < 0
- (1/3) k/a2 + (1/3) c/a4 < 0 , giving a > (c/k)1/2
(b) Intelligent life would be impossible if the orbit were highly elliptical, due to temperature variations as the earth-sun distance varied.
= a (mv2/2) where v is the speed of mass m before the collision,
giving a = [M/(m+M)] (1-e 2) , m/M = [(1 - e 2)/a ] 1
This corresponds to an elastic collision.
xcm = S xi mi / S mi = 0 from symmetry, so C of M is at the center of the rod.
(b) Iz = S mi xi2 = Irod + 2 I sphere
I sphere = M of I about an axis displaced (L/2 + r) from the center of the sphere
= (2/5)L2 + m(L/2+r)2 from the parallel-axis theorem.
Therefore total moment of inertia: Iz= ML2/12 + (2/5)r2 + m(L/2 + r)2
From perpendicular-axis theorem, Iz = Ix + Iy = ma2/6, giving k = a/Ö 6
5. (a) E = 105 eV = 105 e Joule. From Eq.(6.12.9), p. 242,
impact parameter b = [Qq/(2E. 4p e 0.)] cot(60° /2) in SI units
= [(2e)(79e) / (2 x 105 . e . 4p e 0.)] cot(60° /2)
[(158)(1.60x10-19) / (2x105)(1.11 x 10-10)] (1.732)
= 1.97 x 10-12 m
(b) In SI units, ds /dW = [(Ze)(2e)/(4p e 0.4E)]2 / [sin4(60deg/2)]
ds /dW = [2Ze/(4p e 0 . 4x105)]2 / [sin4(30deg)]
= [(158)(1.6 x 10-19)/(4p e 0.4x105)]2 / [sin4(30deg)]
= [(158)(1.6 x 10-19)/(1.11 x 10-10)(4x105)]2 [16]
= [5.70 x 10-13]2 [16] = 5.20 x 10-24 m2/steradian
a:P425mt00.doc