9-17. (Research project on orbital motion)
Assume a mass m located at a position r =reˆr experiences a central force
F=mf (r)ˆer
(a) Show the equation of motion is given by md
(^2) r
dt^2
=F which can be written in the
form dv
dt
=f(r)ˆer
(b) Show that r ×v =his a constant.
(c) Show the motion of mis in a plane and that the mass m sweeps out an area at
a constant rate. (Kepler’s law of areas).
(d) Show that in the special case mf (r) = −
GmM
r^2 the mass mis attracted toward
mass M, assumed to be at the origin, and
dv
dt = −
k
r^2
ˆer where k =GM is a
constant.
(e) Show that h=r^2 ˆer×d
ˆer
dt ,
dv
dt ×
h=kdˆer
dt and v ×
h=k(ˆer+
)where
is a constant
vector.
(f) Use the results from part (e) and show
r ×v ·h=h^2 and r ·v ×h=kr (1 + cos θ)
where θis the angle between
and r , and consequently
r=
α
1 + cos θ, where α=
h^2
k
Note rdescribes a conic section having eccentricity.
(f) When < 1 show an ellipse results with mhaving an orbital period
T=
area of ellipse
h/ 2 =
√^2 π
k
a^3 /^2 , where
T^2
a^3 =
4 π^2
k
This is known as Kepler’s third law.
9-18. (a) Find the potential associated with the conservative vector field
F= (y^2 cos x+z^3 )ˆe 1 + (2 ysin x−4) ˆe 2 + 3 xz^2 ˆe 3
(b) Find the differential equation which describes the field lines.
9-19. Show that the vector field
F = (2xyz +y)ˆe 1 + (x^2 z+x)ˆe 2 +x^2 yeˆ 3