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Chapter 4:

Classical Mechanics

Gerik Scheuermann University of Kaiserslautern

Germany

3

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 : IR3 tr t( ) v : IR3

tv t( ) f=mg

4 We are looking for the particle trace.

Integration gives the well-known result:

x : IR3 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

2

v

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 2

1-

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

v0 r

--t 1 2---gt+v0

= 1 --- rt( ∧r) 1

2--- g( ∧r)t+v0r

= 1

2--- g( ∧r)t=–v0r=rv0 t 2rv0

gr ---

=

(2)

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 t 2rv0

gr --- 2v0

g --- 2v0

---g 0 --- .

= = =

r --t 1

2---gt+v0

= gr=gtv0 r gv0

g

--- t 2 g( ∧v0)(v0) g ( )2 ---

2 g( ∧v0)•(v0) g2 ---

= = =

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) v02

2 a( ∧b)•(bc) =b2(ac)–a•(bcb)

2 gˆ( ∧v0)•(v0) = v02(•(0rˆvˆ0))

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.

0g•(0rˆvˆ0)

•(0rˆvˆ0)

– =1

– =0rˆvˆ0 gˆvˆ0 – =0rˆ .

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– ---

=

v

2

2g

12

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=mgmγv , γ>0 .

=g–γv ⇔ +γv=g .

eγt(+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( )tv0 geγsds 0 t

ge---γtγ1

= =

v t( ) g1–eγt ---γ +v0eγt.

= r=xx0 r geγt+γt–1

γ2

--- v01–e– tγ --- .γ +

=

(3)

14 We are now interested in the time a particle needs to hit the line in direction r.

---r

=

γ > 0

γ = 0

15 We use the formula for the particle trace to obtain the time of flight.

r=2eγt+γt–1+v0γ11–e– tγ |γ2rˆ∧

γ2r=g e(γt+γt–1) γr+ ∧v0(1–eγt) 0=g e( γt+γt–1)+γrˆ∧v0(1–eγt) | : rˆ( ∧g) 0 (eγt+γt–1) γv0

g --- 1 –eγt +

=

γt 1 1

2---γT

 – 

 1–eγt

, T 2v0

g ---.

= =

16 T is the time needed in the case without drag. Fort1, we have

yt 1 1

2---γT

 + 

  γt 1

2---γ2t2

– 1

6---γ3t3

 + 

  | : 1

2---γ2t 1 1 2---γT

 + 

 

 

 

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

r 2eγt+γt–1

v0γ11–e– tγ

| gˆ∧ +

=

r=ˆ2(eγt+γt–1)+v0γ1(1–eγt) r v0

--- 1–eγt

---γ

 

 

=

1–eγt ---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 v0

---T 1 2

3---γT

 – 

 .

R v0 ---T ,

=

r R 1 2

3---γT

 – 

 

R 1

---3v0 ---

 – 

 .

=

(4)

20

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

=

=ω×v .

21 Because of

we get

Rearranging terms, this means

ω×v=–i(ω∧v)=–( )v=v•Ω, Ω=

=v•Ω.

1 2---Ωv 1

2---vΩ

+ =0 .

22 We are looking now for an integrating factor R with

This would allow R1

2---Ω

= 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 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,

RR=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 RvRv0=0 v=Rv0R=e0.5Ωtv0e0.5Ωt.

v=v||+v Ωv||=v||Ω Ωv=–vRv0||=v0||R Rv0⊥=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 |_

(5)

26 For the trajectory, we get

With

we have

xx0 v0⊥1eΩt–1 v0||t . +

=

r=xx0+v0•Ω1=xx0+v0×ω1

r= (v0•Ω1)eΩt+v0||t= (v0×ω1)eiωt+(v0•ω1) ωt .

27 Setting

one gets the standard helix

with

a=v0×ω b=v0•ω θ = ωt θ= θ ωˆ

r( )θ =ae+

a•θ=0

θ ae

a x

0 θ i

b

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