2
Chapter 4:
Classical Mechanics
Gerik Scheuermann University of Kaiserslautern
Germany
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4.1 Constant Force and Single Particle
A single particle is modeled as an object with position and velocity.
A constant force f interacts with the particle.
Here, m is the mass of the particle and g an acceleration of the par- ticle induced by the force.
r : I→R3 t→r t( ) v : I→R3
t→v t( ) f=mg
4 We are looking for the particle trace.
Integration gives the well-known result:
x : I→R3 x 0( )=x0 x˙ 0( ) =v 0( ) =v0
x˙˙ t( )=v˙ t( ) =g x˙ t( ) =v t( ) =gt+v0 r t( ) x t( )–x0 1
2---gt2+v0t
= =
5 The following figure shows the particle trace.
r v t
gt
2v
g v
0
1 -2
0
6 Using the average velocity
we can analyze this also in a v-t diagram, called hodograph.
v r
--t 1 2---gt+v0
= =
v=r/t gt gt
v
_
-v
0 21-
21
7 We want to compute now the range of a target in direction that has been hit by our particle starting with velocity .We have
rˆ v0 r
--t 1 2---gt+v0
= 1 --- rt( ∧r) 1
2--- g( ∧r)t+v0∧r
= 1
2--- g( ∧r)t=–v0∧r=r∧v0 t 2r∧v0
g∧r ---
=
8 This is independent from the absolute value of r. If the unit direc- tion of our target is , the time needed to hit the target is
The range can now be computed by rˆ t 2r∧v0
g∧r --- 2rˆ∧v0
g∧rˆ --- 2v0
---g rˆ∧vˆ0 gˆ∧rˆ --- .
= = =
r --t 1
2---gt+v0
= g∧r=gt∧v0 r g∧v0
g∧rˆ
--- t 2 g( ∧v0)(rˆ∧v0) g∧rˆ ( )2 ---
2 g( ∧v0)•(v0∧rˆ) g∧rˆ2 ---
= = =
9 The term in the numerator
can be used to maximize the range for a fixed direction and a fixed absolute velocity . The general identity
gives
g 2 gˆ( ∧v0)•(v0∧rˆ) rˆ v02
2 a( ∧b)•(b∧c) =b2(a•c)–a•(bcb)
2 gˆ( ∧v0)•(v0∧rˆ) = v02(gˆ•rˆ–gˆ•(vˆ0rˆvˆ0))
10 For a variation of , we have to maximize . Since the brackets contain a unit vector like , we have to solve
This means that the angle between and equals the angle between and r.
vˆ0 –g•(vˆ0rˆvˆ0) gˆ
gˆ•(vˆ0rˆvˆ0)
– =1
gˆ – =vˆ0rˆvˆ0 gˆvˆ0 – =vˆ0rˆ .
g v0
v0
g
r-g ^
v ^ 0
r ^
^
^
11 With more calculations, we get a formula for the maximal range.
This is a paraboloid of revolution.
rmax v0 ---g 1
1–gˆ•rˆ ---
=
v
22g
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4.2 Constant Force with Linear Drag
A linear resistance in the direction of the velocity of a particle is also called linear drag. The force on the particle is now
The velocity is given by
This can be solved by using
F=mg–mγv , γ>0 .
v˙=g–γv ⇔ v˙+γv=g .
eγt(v˙+γv) d dt--- ve γt
geγt.
= =
13 For a particle with starting velocity , this gives
For the displacement , we integrate to get v0
v t( )eγ( )t –v0 geγsds 0 t
∫
ge---γtγ–1= =
v t( ) g1–e–γt ---γ +v0e–γt.
= r=x–x0 r ge–γt+γt–1
γ2
--- v01–e– tγ --- .γ +
=
14 We are now interested in the time a particle needs to hit the line in directionrˆ r.
---r
=
γ > 0
γ = 0
15 We use the formula for the particle trace to obtain the time of flight.
r=gγ–2e–γt+γt–1+v0γ–11–e– tγ |γ2rˆ∧
γ2rˆ∧r=rˆ∧g e(–γt+γt–1) γr+ ∧v0(1–e–γt) 0=rˆ∧g e( –γt+γt–1)+γrˆ∧v0(1–e–γt) | : rˆ( ∧g) 0 (e–γt+γt–1) γrˆ∧v0
rˆ∧g --- 1 –e–γt +
=
γt 1 1
2---γT
–
1–e–γt
, T 2rˆ∧v0
g∧rˆ ---.
= =
16 T is the time needed in the case without drag. Fort<γ–1, we have
yt 1 1
2---γT
+
γt 1
2---γ2t2
– 1
6---γ3t3
+
| : 1
2---γ2t 1 1 2---γT
+
≈
2γ–11 1 2---γT
+
–1 2
γ---–t 1 3---γt2
≈ +
t
2 1 1
2---γT
+
γ1 1 2---γT
+
--- 2 γ1 1
2---γT
+
---
– 1
3---γt2 | t2
+ T2
≈ ≈
t T
1 1
2---γT + --- 1
3---γT2
≈ +
17 Further approximation gives
t T 1 1
2---γT
–
1
3---γT2
≈ +
t T 1 1
6---γT
–
≈
18 The intersection can now be computed by taking the outer product of the displacement equation with .
With
gˆ r gγ–2e–γt+γt–1
v0γ–11–e– tγ
| gˆ∧ +
=
gˆ∧r=gˆ∧gγˆ–2(e–γt+γt–1)+gˆ∧v0γ–1(1–e–γt) r gˆ∧v0
gˆ∧rˆ --- 1–e–γt
---γ
=
1–e–γt ---γ t 1
2---γt2
– T 1 1
6---γT
–
1
2---γT2
≈ ≈ – T 1 2
3---γT
–
=
19 we have
Using the range without drag
we find finally the range as r gˆ∧v0
gˆ∧rˆ ---T 1 2
3---γT
–
.
≈
R gˆ∧v0 gˆ∧rˆ ---T ,
=
r R 1 2
3---γT
–
≈ R 1 4γ
---3rˆ∧v0 gˆ∧rˆ ---
–
.
=
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4.3 Constant Magnetic Field
The usual description for the interaction between a charged particle with charge q and mass m is
With , we have
mv˙ q
---vc ×B.
=
ω q
mc---
–
B
=
v˙=ω×v .
21 Because of
we get
Rearranging terms, this means
ω×v=–i(ω∧v)=–( )iω •v=v•Ω, Ω=iω
v˙=v•Ω.
v˙ 1 2---Ωv 1
2---vΩ –
+ =0 .
22 We are looking now for an integrating factor R with
This would allow R˙ R1
2---Ω
= R˙† 1
2---ΩR† –
=
d
dt--- RvR( †) dR ---vRdt † Rdv
dt---R† RvdR† ---dt
+ +
= =
R1
2---ΩvR† Rv˙R† Rv 1 2---ΩR†
–
+ + =
R 1 2---Ωv v˙ 1
2---vΩ –
+
R†=0
23 Since we have a constant magnetic field and , we set
and find
Ω=const.
R t( ) e 1 2---Ωt
=
R†( )t e 1 2--- – Ωt
,
= R 0( ) =R†( )0 =1,
R†R=RR†=1.
24 For the velocity, we have
Separating v into parallel and orthogonal parts with respect to the magnetic field shows
d dt--- RvR( †) =0 RvR†–v0=0 v=R†v0R=e–0.5Ωtv0e0.5Ωt.
v=v||+v⊥ Ωv||=v||Ω Ωv⊥=–v⊥Ω R†v0||=v0||R† R†v0⊥=v0⊥R
25 This results in
This shows that the parallel velocity is constant and that the orthogonal velocity rotates through an angle in time, so v sweeps out a portion of a cone.
v=v0⊥R2+v0||=v0⊥eΩt+v0||.
Ωt
v
0|| v
v
Ω ω
0
0 |_
26 For the trajectory, we get
With
we have
x–x0 v0⊥Ω–1eΩt–1 v0||t . +
=
r=x–x0+v0•Ω–1=x–x0+v0×ω–1
r= (v0•Ω–1)eΩt+v0||t= (v0×ω–1)eiωt+(v0•ω–1) ωt .
27 Setting
one gets the standard helix
with
a=v0×ω b=v0•ω θ = ωt θ= θ ωˆ
r( )θ =aeiθ+bθ
a•θ=0
θ ae
a x
0 θ i
b