Central Forces - Classical Mechanics - Lecture Slides, Slides of Classical Mechanics

These key points are discussed in these slides of classical mechanics : Central Forces, Two-Body System, Reduced Mass, Smaller Mass, Central Motion, Momentum, Orbital Angular, Velocity, Coplanar, Perpendicular

Typology: Slides

2012/2013

Uploaded on 07/24/2013

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Central

Forces

Two

‐Body

System

•^

Center

of

mass

R

•^

Equal

external

force

on

both

bodies.

•^

Add

to

get

the

CM

motion

•^

Subtract

for

relative

motion ext 1

int 1 (^11)

F

F

r m^

^ 

m^2

r^1

F^2

int r^2

R^

m^1

F^1

int

F^1

ext

F^2

ext^

r = r

- r 1

2

ext 2

int 2 (^22)

F

F

r m^

^ 

ext 2

ext 1

F

F

R

M

^ 

int 2 2

int 1 1 2 1

F m

F m r r

^ 

^ 

Central

Motion

•^

Central

motion

takes

place

in

a

plane.

-^

Force,

velocity,

and

radius

are

coplanar.

•^

Orbital

angular

momentum

is

constant.

•^

If

the

central

force

is

time

‐independent,

the

orbit

is

symmetrical

about

an

apse.

-^

Apse

is

where

velocity

is

perpendicular

to

radius

r r r r Jd dt

r r p r J

^ 

^

Use

J^

to avoid confusion

with Lagrangian

L

Central

Force

Equations

•^

Use

spherical

coordinates.

-^

Makes

r^ obvious

from

central

force.

-^

Generalized

forces

Q

=  Q

= 

-^

Central

force

need

not

be

from

a

potential.

-^

Kinetic

energy

expression

sin

(^

2 2 2 2 2 2

1 2

^

^

r

r r

T^

Q^ r T r T r d^ dt

^ 

T

T

d dt

T

T

d dt

Angle

Equation

•^

T^

doesn’t

depend

on

^ directly.

•^

Also

represents

constant

angular

momentum.^ –

A

constant

of

the

motion

•^

Change

the

time

derivative

to

an

angle

derivative.

T

T

d dt

T 

d dt

J

r T^

^

2

constant^ 

d d J r

d d d dt d^ dt

2 

Orbit

Equation

Let

u

= 1/

r

Qr T r T r d^ dt

^ 

Q^ r T r T r d d J^ r

^ 

^

2

Q^ r

r

r r

r

r r

d d J^ r

^

)]

[

)]

[^

2 2 2 1 2

2 2 2 1 2

2

Q^ r J r

dr d J r d d J r

J r r rd d J^ r

^

2 3

2

2 2 2

2

2

3

2

2

Q J

r

dr d r d d r

r

^

^

2 2

2 2

u Q J

u

d

u d^

r

^

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