Euler-Lagrange Equations and Magnetic Fields: Helix Trajectories and Drift Velocities - Pr, Assignments of Physics

The euler-lagrange equations of motion for a charged particle in an electromagnetic field, focusing on the calculation of the trajectories in different frames and the analysis of the drift velocities. Topics such as lorentz transformations, euler-lagrange equations, and magnetic fields. Students studying classical electrodynamics or physics may find this document useful for understanding the behavior of charged particles in various frames and the role of electric and magnetic fields in their motion.

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Pre 2010

Uploaded on 09/17/2009

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Hw6, 12.1, 12.5, 12.6, 12.9, 12.14
12.1
The Euler-Lagrange equations of motion are
d
∂L
∂uβL
∂xβ= 0
From
L=m
2uαuαq
cuαAα
we can calculate ∂L
∂uβ=muβq
cAβ
and ∂L
∂xβ=q
cuα
∂Aα
∂xβ
Now plugging these results into the Euler-Lagrange equations yields
d
muβq
cAβ=q
cuα
∂Aα
∂xβ
md2xβ
2=q
cdAβ
uα
∂Aα
∂xβ
=q
cβAααAβdxα
12.5
a) E < B
Following section 12.3, we boost into K’ frame moving relative to the lab frame at velocity
u=cE×B
B2
The E-field vanishes in K’ frame, leaving only the uniform B-field
B=B2E2
B21/2
Bˆy
The trajectory in this frame is, as done in section 12.2, a helix winding around the B-field
~x(t) = vktˆ
y+Re ia(ˆ
xiˆ
z)exp(Bt)
We now boost back into the lab frame using equation 11.18 to obtain
x(t) = acos(ωBt)
y(t) = vkt
z(t) = γ(asin(ωBt) + ut)
pf3
pf4
pf5

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Hw6, 12.1, 12.5, 12.6, 12.9, 12.

The Euler-Lagrange equations of motion are

d dτ

∂L

∂uβ

∂L

∂xβ^

From L = −

m 2

uαuα −

q c

uαAα

we can calculate ∂L ∂uβ^

= −muβ −

q c

and ∂L ∂xβ^

q c

∂Aα ∂xβ

Now plugging these results into the Euler-Lagrange equations yields

d dτ

−muβ −

q c

q c

∂Aα ∂xβ

−m

d^2 xβ dτ 2

q c

dAβ dτ

− uα

∂Aα ∂xβ

q c

∂β^ Aα^ − ∂αAβ^

) (^) dxα dτ

a) E < B Following section 12.3, we boost into K’ frame moving relative to the lab frame at velocity

u = c

E × B

B^2

The E-field vanishes in K’ frame, leaving only the uniform B-field

B′^ =

B^2 − E^2

B^2

B yˆ

The trajectory in this frame is, as done in section 12.2, a helix winding around the B-field

~x(t) = v‖t yˆ′^ + Re

ia( ˆx′^ − i zˆ′)exp(−iωB′ t)

We now boost back into the lab frame using equation 11.18 to obtain

x(t′) = a cos(ωB′ t′) y(t′) = v‖t′ z(t′) = γ (a sin(ωB′ t′) + ut′)

where

γ =

1 − (u/c)^2

and

a =

cp′⊥ eB′

Note that t′^ is not the time in the lab frame. It is acceptable nonetheless because we just want a parametric expression for the trajectory. So, in the lab frame the particle makes a helix with the same circular frequency while uniformly translating along a line in the yz plane. b) E > B We boost into frame K’ at velocity

u = c

E × B

E^2

We have only a uniform E-field in this frame. We have encountered this situation in our last homework. We showed that the particle moves with increasing speed in the direction of the E-field. The mass gets heavier, and the velocity component perpendicular to the field becomes smaller over time. Taking our results from 12.3, we can then boost back into the lab frame.

x(t′) =

mc^2 γ 0 eE′

eE′t′ mcγ 0

y(t′) =

mcγ 0 eE′^

v 0 sin φ 0 sinh−^1

eE′t′ mcγ 0

z(t′) = γ

mcγ 0 eE′^

v 0 sin φ 0 sinh−^1

eE′t′ mcγ 0

  • u′t′

From our last homework, we know we can boost into a frame K’ in which E′^ and B′^ are parallel, thus reducing to part b of the question. Choosing E′^ and B′^ to be in the z-direction, we have a system of 2nd order ODEs

duα dτ

e mc

F αβ^ uβ

Expanding these equations leads to

du^0 dτ

eE mc

u^3 du^3 dτ

eE mc

u^0

du^1 dτ

eB mc

u^2

du^2 dτ

eB mc

u^1

We see that the 0 and 3 components will behave like sinh(ρφ) and cosh(ρφ) whereas 1 and 2 like sin(φ) and cos(φ). This is typical of these problems: the E-field generates an asymptotic

and we do not have curvature drift. On the other hand, we will have the gradient drift due to |B| changing in the r and φ directions. From

▽⊥|B| = ˆr

∂B

∂r

  • φˆ

r sin θ

∂B

∂φ

= −

3 M

r^4

ˆr

we have for the drift velocity

vG = −

3 a^2 ωB 2 r

φˆ

Because a ≪ R,

vG = R φ˙ ≈ −

3 a^2 ωB 2 R

c) From equation 12.

(v‖)^2 = (R θ˙)^2 = v 02 − v^2 ‖ 0

B(z) B 0

Let θ = π/2 + ǫ. From expanding B about θ = π/2 and differentiating the equation above with respect to time, we obtain

ǫ¨ = −

v^2 ‖ 0 2 R^5

9 M

B 0

ǫ

Hence, the frequency at which θ oscillates about π/2 is

ωB

a R

The Euler-Lagrange equation is

∂μ^

∂L

∂(∂μAν^ )

∂L

∂Aν

where

L = −

8 π

∂αAβ ∂αAβ^ −

c

JαAα

Straightforward differentiation yields

∂μ∂μAν =

4 π c

Recall from equation 11.141 that Maxwell’s equations are

∂μ(∂μAν^ − ∂ν^ Aμ) =

4 π c

Hence, our Euler-Lagrange equation becomes Maxwell’s equations if

∂μAμ = 0

b) Straightforward calculation shows the difference between the Lagrangian in part a and that given in 12.85 is

L 12. 85 − La =

8 π

∂ν (Aμ∂μAν^ )

which clearly is a 4-divergence. Hence, by Stokes theorem the difference in the action is a boundary term, which is kept constant. Therefore, the equations of motion remain the same.