rotational motion 2009 7
TRANSCRIPT
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18_12afig_PChem.jpg
Rotational Motion
Center of Mass
Translational Motion
r1
r2
2
2H
m
2
2H
I
L L
22
( )2 2 eqk
H
r r
Motion of Two Bodies
Each type of motion is best represented
in its own coordinate system best suited
to solving the equations involved
w
k
2 22 2
1 2 1 2
1 2
( , )2 2H Vm m r r
RcInternalcoordinates
Cartesian
Internal motion (w.r.t CM)
Motion of the C.M.
2r
1r
Origin
r
Vibrational Motion
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Centre of Mass
1 1 2 2 1 1 1 1 2 2 2 21 2
, , , , , ,m m
X Y Z x y z x y zm m
r rR r r
Weighted average of all positions
1 1 2 2
1 2
m x m xX
m m
1 1 2 2
1 2
m y m yY
m m
1 1 2 2
1 2
m z m z Z
m m
2 22 2
( ) ( ) ( )2 2H H H VM R rR r r
Motion of Two Bodies
Internal Coordinates:
1 1 2 2& r r R r r R 1 2 r r r
1 2 1 2 r r R r R r r
In C.M. Coordinates:
( , , )x y zr
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Kinetic Energy Terms
2 22 2
( ) ( ) 2 2K K K M R rR r
? ?
2 2 2 2 2
22 2 2
( )2 2
d d dKM M dX dY dZ
RR
2 2 2 2 22
2 2 2 ( )
2 2
d d dK
dx dy dz
rr
? ? ?
? ? ?
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Centre of Mass Coordinates
1 1 1
d dX d dx d
dx dx dX dx dx
1 1 2 2 1 1
1 1 1 2 1 2
m x m x m mdX d
dx dx m m m m M
1 21 1
1dx d
x xdx dx
1
1
md d d
dx M dX dx
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Centre of Mass Coordinates
2 2 2
d dX d dx d
dx dx dX dx dx
1 1 2 2 2 2
2 2 1 2 1 2
m x m x m mdX d
dx dx m m m m M
1 22 2
1dx d
x xdx dx
2
2
md d d
dx M dX dx
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Centre of Mass Coordinates
2
1 12
1
m md d d d d
dx M dX dx M dX dx
2 2 2
1 1 1
2 2 2
m m md d d d d d
M dX M dX dx dx M dX dx
22 2 2
2 2
2 2 2 2
2
2m md d d d
dx M dX M dXdx dx
Similarly
2 2 2
1 1
2 2 2
2m md d d
M dX M dXdx dx
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Centre of Mass Coordinates
2 2 2
1
2 2 2 2
1 1 1
1 2 1md d d d
m dx M dX M dXdx m dx
2 22 2 2 2
1 2 2 2
1 2 1 1 2 2
1 1
2 2x xx
d dK m m m dx m dx
2 2 2
2
2 2 2 2
2 2 2
1 2 1md d d d
m dx M dX M dXdx m dx
2 2 2 2 2 2
1 2
2 2 2 2 2 2 2 2
1 1 2 2 2 1
1 1 1 1m md d d d d d
m dx m dx M dX M dX m dx m dx
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Centre of Mass Coordinates
2 2 2 2
1 2
2 2 2 2 2 2
1 1 2 2 1 2
1 1 1 1m md d d d
m dx m dx M M dX m m dx
2 2
2 2
1 1d d
M dX dx 1 2
1 2 1 2
1 1 1 m m
m m m m
Reduced mass2 2 2
2 2
1 1
2x
d dK
M dX dx
2
2 2internal1 1
2CMK K K
M R r
2 2 22
2 2 2
d d d
dX dY dZ
R
2 2 22
2 2 2
d d d
dx dy dz
r
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Hamiltonian2 2
2 2
( ) ( ) ( )2 2H H H VM R rR r r
( , ) ( ) ( ) ( ) ( ) ( ) ( )H H H E E R rR r R r R r R r
( ) ( ) ( )H E RR R R
22 ( ) ( ) ( )
2
V E
r rr r r
22 ( ) ( )
2E
M R RR R
( ) ( ) ( )H E rr r r
C.M. Motion
3-D P.I.B
Internal Motion
Rotation
Vibration
Separable!
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Rotational Motion and Angular Momentum2
2 ( ) ( )
2
K
rr r We rotational motion to internal coordinates
i i
i
p m v
Linear momentum of a rotating Body
i ii
p m rw
i i
dv r
dt
Ds
is r D Didsvdt
i iv rw
d
dt
w
f
Angular Velocity
Parallel to moving body
p(t1)
p(t2)
Always changing direction with time???
Always perpendicular to r
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Angular Momentum
L r p
v
m
r
p
L
L r p
f
sinf r p r p
Perpendicular to R and p
Orientation remains constant with time
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Rotational Motion and Angular Momentum
i ii
L r p
IwL
2
i i
i
m w r
2i i
i
m w
r
2
i i
i
I m rMoment of inertia
As p is always perpendicular to r
2 r r r r r
r
Center
of mass
R
1r
2r
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Rotational Motion and Angular Momentum
1 2 1 2 r r r r r
2 2
1 1 2 2I m m r r
r
Center
of mass
R
1r
2r
2 2
1 1 2 2m m r R r R
2 21 2m m
M M r r r
1 1 2 21 1 1 1 2 1 1 1 2 2
1m mMm m m m
M M M
r rr R r r r r r
2
21 2
1 2
1 1 m mm m M
r
2 221
r r
1 12 2 1m m
M M r R r r r
2 22 22 1
1 2
m mI m m
M M
r r
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Rotational Motion and Angular Momentum
Classical Kinetic Energy
2
. .2
i
i i
pK E
m
22
2 2
i ii i
i i
m rm v w
222
2 2 2
LII
I I
ww
2 22 2
2 2i i
i
m rw w
r
r
Centerof mass
R
1
r
2r
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Rotational Motion and Angular Momentum
2
. . 2
L
K E I
21 2
K LI
22
2K
r
2
( ) ( )2
LK
I r r
22 ( ) ( )
2K
rr r
L i r r
2 r rr r Sincer and p areperpendicular
r
Center
of mass
R
1r
2r
2 2
2 2 2 2 IL
r r r rr r r r
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Momentum Summary
21
2K r p
I
22
2K
L i r
Linear
Classical QM
Rotational
(Angular)
Momentum
Energy
Momentum
Energy 2
2
2K r
I
p i
L r p
drp mv m
dt
2 2
22 2
p m d r
K m dt
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Angular Momentum
L r p
x y zx y z p p p L
x y z
x y z
p p p
i j k
L
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Angular Momentum
x y zL L L L i j k
x z y
y x z
z y x
L yp zp
L zp xp
L xp yp
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Angular Momentum in QM
( ) ( ) ( ) ( )
( ) ( )
x x z y
y y x z
z z y x
L L yp zp
L L zp xp
L L xp yp
r r
r r
r r
x
y
z
d dL i y z
dz dy
d dL i z xdx dz
d dL i x y
dy dx
x y zL L L
L i j k
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Angular Momentum
i L r p r
d d d
x y z i dx dy dz
L
i x y z
d d d
dx dy dz
i j k
L
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Angular Momentum
x y zL L L L i j k
x
y
z
d dL i y zdz dy
d dL i z x
dx dz
d dL i x y
dy dx
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Two-Dimensional Rotational Motion
cos( )x r f
x
y
fr
sin( )y r f
d d
dx dy
i j
How to we get:
( , ) ( , )d d
r rdx dy
f f
i j
Polar Coordinates
cos( ) sin( )d dx d dy d d d dr dr dx dr dy dx dy
f f
sin( ) cos( )d dx d dy d d d
r r
d d dx d dy dx dy
f f
f f f
2 22
2 2
d d
dx dy
2 22
2 2( , ) ( , )
d dr r
dx dyf f
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Two-Dimensional Rotational Motion
cos( ) sin( )d dx d dy d d d
dr dr dx dr dy dx dyf f
d d dr x y
dr dx dy
2 2
1 d x d y d
r dr r dx r dy
2 2
1 d d x d y d d d
r x yr dr dr r dx r dy dx dy
2 2 2 2
x d d x d d y d d y d dx y x y
r dx dx r dx dy r dy dx r dy dy
2 2 2 2
2 2 2 2 2 2 2 2
x d x d xy d yx d y d y d
r dx r dx r dxdy r dydx r dy r dy
2 2 2 2
xx d d xy d d yx d d y dy d d dy
r dx dx r dx dy r dy dx r dy dy dy dy
product rule
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Two-Dimensional Rotational Motion
sin( ) cos( )d dx d dy d d d d d
r r y xd d dx d dy dx dy dx dy
f ff f f
2
2
d d d d d y x y x
d dx dy dx dyf
2 22 2
2 2
d dx d d d d d d d y y yx x xy x
dx dx dy dx dy dx dy dx dy
d d d d d d d d y y y x x y x x
dx dx dx dy dy dx dy dy
2 2 2 2 2
2 2 2 2 2 2 2 2 2 2
1 d y d y d yx d x d xy d x d
r d r dx r dy r dxdy r dx r dydx r dyf
2 22 2
2 2
d d d d d d y y yx x xy x
dx dy dxdy dx dydx dy
product rule
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Two-Dimensional Rotational Motion
2 2 2 2
2 2 2 2 2 2 2 2
1 d d x d x d xy d yx d y d y d r
r dr dr r dx r dx r dxdy r dydx r dy r dy
2 2 2 2 2
2 2 2 2 2 2 2 2 2 2
1 d y d x d yx d xy d y d x d
r d r dx r dx r dxdy r dydx r dy r dyf
2 2 2 2 2 2 2 2 2
2 2 2 2 2 2 2 2 2 2
1 1d d d x d y d x d y d r
r dr dr r d r dx r dx r dy r dyf
2 2 2 2 2 2
2 2 2 2 2 2x y d x y dr r dx r r dy
2 22
2 2
d d
dx dy
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Two-Dimensional Rotational Motion
2
2
2 21 1d d dr
dr r dr r d f
2 2 2
2 2 2 2
1 1d d d d d r
dr r dr r d dx dyf
2 2 2
22 2
1 1
2 2
d d dH rdr r dr r d f
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Two-Dimensional Rigid Rotor
22
( , ) ( , ) ( , )2H r r E r f f f
Assume ris rigid, ie. it is constant
2 2 22
2 2
1 1
2 2
d d dH r
dr r dr r d f
2 2 22
2 2
1
2 2r
dH
r d f
2
2
zLHI
z rd
L i idf
As the system is rotating about the z-axis
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18_05fig_PChem.jpg
Two-Dimensional Rigid Rotor
2 2
2( ) 0
2
dE
I d f
f
2
2 2
2( ) 0
d IE
d f
f
2
22 ( ) 0d kd
f
r
2 22
2
2
2
I kk E
I
2 2
2 ( ) ( ) ( )
2
dH E
I d
f f f
f
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18_05fig_PChem.jpg
Two-Dimensional Rigid Rotor
22
2 ( ) 0
d
kd ff
( ) 0d d
ik ik
d d
f
f f
( ) 0 & ( ) 0d d
ik ik d d
f f f f
( ) ikA e f f ( )ikA e f f
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18_05fig_PChem.jpg
Two-Dimensional Rigid Rotor
( ) ikA e f f
Periodic
2 2 2 2
2 2 m
k m
E EI I
2( 2 ) ( )
ik ikA e A ef f f f
2 1 2 2ik
e k m k m k
m = quantum number
( ) imm A ef f ( )
im
m A ef f
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18_05fig_PChem.jpg
Two-Dimensional Rigid Rotor
( ) imm A ef f
2 2 22
2
2 2r
dH
I d f
z r
dL i i
df
2 2 ( ) ( )
2m m
mHI
f f
2 2
2
m
mE
I
( ) ( )z m mL m f f
22 2
2
dL
df
2 2 2 ( ) ( )m mL m f f
z mL m
2 2 2
mL m
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Two-Dimensional Rigid Rotor
( ) imm A ef f ( ) ( )m mH E f f
2 2
2m
mE
I
( ) ( )z m mL m f f
z mL m
E
mz mLmEm
6
5
4
3
21
2
I
18.0
12.5
8.0
4.5
2.00.5
6
5
4
3
2
6
5
4
3
21
Only 1 quantum number is require to determine the state of the system.
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Normalization
( ) imm A ef f
2 2* *
0 0( ) ( ) 1 & ( ) ( ) 1m m m m
f f f f
** *( ) im imm A e A e
f f f
( ) imm A ef f
*A A
*
( ) ( )m m f f
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Normalization
2 2*
0 0
1 ( ) ( ) ( ) ( )m m m m
d d
f f f f f f
2 2 2
2 2
0 0 0
1 1 [2 ]im im im imA A e e d A A e e d A d A
f f f f f f f 1
2A
1( )
2
im
m ef f
1( )
2
im
m ef f
2 2
*
0 0
( ) ( ) ( ) ( ) 1m m m md
f f f f f
O h li
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18_06fig_PChem.jpg
1( )
2
im
m ef f
Orthogonality
2
*
,
0
( ) ( )m m m md
f f f *2
0
1 1
2 2
im ime e d
f f f
2
0
1
2
im ime e d
f f f
m = m 2
0
1 21 1
2 2d
f
mm
2 2
0 0
1 1
cos( ) sin( )2 2
i m m
e d m m i m m d
f
f f f f
2 2
0 0
1cos( ) sin( )
2 2
im m d m m d
f f f f
1
0 0 02 2
i
S h i l P l C di t
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14_01fig_PChem.jpg
x y z r i j k
sin cos sin sin cosr r r f f r i j k
Spherical Polar Coordinates
d d d
dx dy dz i j k
( , , ) ( , , ) ( , , )d d d
r r rdx dy dz
f f f
i j k
( , , ) ( , , )
( , , )
x r y r
z r
f f
f
r i j
k
?
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14_01fig_PChem.jpg
sin cos sin sin cosx r y r z r f f
Spherical Polar Coordinates
d dx d dy d dz d
dr dr dx dr dy dr dz
cos sin sin sin cosd d d d
dr dx dy dz f f
cos cos sin cos sind d d d
r r rd dx dy dz
f f
sin sin cos sind d d
r rd dx dy
f f f
.... & ....d d
d d f
Th G di i S h i l P l C di
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14_01fig_PChem.jpg
The Gradient in Spherical Polar Coordinates
cos sin sin sin cos
cos cos sin cos sin
sin sin cos sin 0
d d
dr dx
d dr r r
d dyr rd d
d dz
f f
f f
f f
f
.SP Cart WGradient in Spherical Polar
coordinates expressed in
Cartesian Coordinates
Th G di t i S h i l P l C di t
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14_01fig_PChem.jpg
The Gradient in Spherical Polar Coordinates
cos cos sincos sin sin
sin cos cossin sin
sin
sincos 0
Cart
d d
dx r r dr
d d
dy r r d
ddr ddz
f ff
f ff
f
1
.Cart SP
WGradient in Cartesian
coordinates expressed inSpherical Polar Coordinates
Th G di t i S h i l P l C di t
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14_01fig_PChem.jpg
The Gradient in Spherical Polar Coordinates
1
.
cos cos sincos sin
sin
sin cos cossin sinsin
sincos
Cart SP
d d dd
dr r d r d dx
d d d d
dy dr r d r d
d dd
dr r d dz
f ff
f
f ff f
W
.
Carti
L r
1SPi
L r W
Th G di t i S h i l P l C di t
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14_01fig_PChem.jpg
The Gradient in Spherical Polar Coordinates
cos cos sincos sin
sincos( )sin( )sin cos cos
sin( ) sin( ) sin sinsin
cos( )sin
cos
d d d
dr r d r d rd d d
i rdr r d r d
rd d
dr r d
f ff
ff f f
f f f
x y zL L L L i j k
cos sin cos
sin
cos
cos sinsin
x
y
z
d dL i
d d
d d
L i d d
dL i
d
f f
f
f f f
f
i L r
Th L l i i S h i l P l C di t
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14_01fig_PChem.jpg
The Laplacian in Spherical Polar Coordinates
22 2
2 2 2 2 2
1 1 1
sinsin sin
d d d d d
rr dr dr r d d r d f
22
2
1 .....d rr dr
OR OR2
2
2
2....
d d
dr r dr
Radial Term Angular Terms
2 1 1
Cart SP SP
W W
Th Di i l Ri id R t
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Three-Dimensional Rigid Rotor
Assume ris rigid, ie. it is constant. Then all energy is from rotational motion only.
2 2 2 2 22
. 2 2 2
2 2Cart
d d dH dx dy dz
2 2 22
2 2 2 2
1 1 1 sin
2 2 sin sin
SP
d d d d dH r
r dr dr r d d r d
f
2 2
2 2 2
1 1
sin2 sin sin
d d d
H r d d d f
2
2IL
22 2
2 2
1 1 sin
sin sin
d d dL
d d d
f
Th Di i l Ri id R t
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18_05fig_PChem.jpg
Three-Dimensional Rigid Rotor
2 2
2 2
1 1 ( , ) sin ( , ) ( , )
2 sin sin
d d dH E
I d d d f f f
f
2 2
2 2
1 1sin ( ) ( ) ( ) ( )
2 sin sin
d d dE
I d d d f f
f
22
2sin sin ( ) ( ) ( ) ( ) sin ( ) ( )
d d d
d d d
f f f
f
2
2
2
2
IEE
I
Separable?
Th Di i l Ri id R t
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Three-Dimensional Rigid Rotor
22
2
1( )
( )
dk
df
f f
2 21 sin sin ( ) sin( )
d dk
d d
22
2( )sin sin ( ) ( ) ( ) sin ( ) ( )
d d d
d d df f f f
22
2
1 1sin sin ( ) sin ( )
( ) ( )
d d d
d d d
f
f f
Two separateindependent
equations
k2= separation
Constant
Th Di i l Ri id R t
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18_05fig_PChem.jpg
Three-Dimensional Rigid Rotor
22
2 ( ) 0d
kd ff
1( )
2
im
m eff
1( )
2
im
m eff
k m k
22
2
1
( )( )
d
kd ff f
Recall 2D Rigid Rotor
Th Di i l Ri id R t
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18_05fig_PChem.jpg
Three-Dimensional Rigid Rotor
2 21 sin sin ( ) sin
( )
d dm
d d
2 2sin sin sin ( ) ( )d d
md d
, ( ) cos( )mm
l m l l C P
This equation can be solving using a series expansion, using a Fourier Series:
Where ( 1)l l 2
2 ( 1)
2 2
l
l lE E
I I
Legendre polynomials
2 2sin sin ( ) sin ( ) ( )d d
md d
Th Di i l Ri id R t
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Three-Dimensional Rigid Rotor
2 ( 1)
2l
l lE
I
2 2
2 2
1 1sin ( , ) ( , )
2 sin sin
d d dE
I d d d
f f
f
1( )
2
im
m eff
, , ( ) ( ) ( ) ( )l m m l l m mH E f f , ( ) (cos( ))
mm
l m l l C P
21 ( 1) 1 (cos( )) (cos( ))22 2
m mm im m im
l l l l
l lH C P e C P e
I
f f
,
1( , ) (cos( ))
2
mm im
l m l l Y C P ef f
Spherical Harmonics
, , ( , ) ( , )l m l l mHY E Y f f
Th S h i l H i
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The Spherical Harmonics
,
1( , ) (cos( ))
2
mm im
l m l l Y C P ef f
, 1,..., 1,m l l l l
1/2
(2 1)( )!for 0
2( )!
m
l
l l mC m
l m
1/2
(2 1)( )!( 1) for 0
2( )!
m m
l
l l mC m
l m
For l=0, m=0
21(cos ) (cos 1)2 ! (cos )
l
l
l l
dP
l d
(cos ) sin (cos )(cos )
m
m ml l
dP Pd
0
2 0
0
1(cos ) (cos 1) 1
2 0! (cos )l
dP
d
0
0 0
0 (cos ) sin 1 1(cos )
d
P d
The Spherical Harmonics
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The Spherical Harmonics
,
1( , ) (cos( ))
2
mm im
l m l l Y C P ef f
0
0 (cos( )) 1P
0
0,0
1 1 1( , ) (1)
2 2 2
iY e f
For l=0, m=0
1/2
0 (2* 0 1)(0 0)! 1( 1)2(0)! 2
mlC
0,0
1
, (0, ), (0,2 )2 oY r r f
Everywhere on the surface of the
sphere has value 1
2
what is ro ? r = (ro, , f
The Spherical Harmonics
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The Spherical Harmonics
r = (1, , f
Normalization:
*
0,0 0,0
S
Y Y dV
2 sin( ) sin( )o
dV dxdydz
r d d d d f f
*( ) ( , )
( ) ( , )
1 11
2 2
f o f j f f f
i o i i i i i
x r y f x z g x y
x r y f x y g x y
dxdydz
2 2 2 2Where ox y z r
*2
0 0
1 1 sin( )2 2
d d
f
In Spherical Polar Coordinates
2
0 0
1sin( )
4d d
f
2
0 0
1sin
4d d
f
2
0 0
1 1cos 2(2 ) 1
4 4
f
1or
r is fixed at ro.
The wavefunction is an angular
function which has a constant valueover the entire unit circle.
X
Y
Z
1
2
The Spherical Harmonics
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The Spherical Harmonics
01,01 3 3
( , ) 1 cos( ) cos( )22 2
iY e f f
1,0
3( ) cos( )
2
(0, ), (0, 2 )
Y
f
r = (1, , f
X
Y
Z
The wavefunction is an angular
function which has a value varying ason the entire unit circle.
3cos( )
2
The spherical Harmonics
are often plotted as a
vector strating from the
origin with orientation
and f and its length is
Y(,f)
Along z-axis
2 1
1 1
1(cos ) (cos 1) cos
2 1! (cos )
dP
d
0
0 0
1 (cos ) sin cos cos(cos )
dPd
For l=1, m=0
The Spherical Harmonics
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18_05fig_PChem.jpg
The Spherical Harmonics
1, 1
3( , ) sin( )
2 2
iY e f f
Complex Valued??
1, 1 1, 1
1 3 3( , ) ( , ) sin( ) sin( ) cos( )
2 4 2 2 2
i iY Y e ef f f f f
Along x-axis
1, 1 1, 1
1 3 3( , ) ( , ) sin( ) sin( )sin( )
2 4 2 2 2
i iY Y e ei i
f f f f f
Along y-axis
1
1 1
1 1(cos ) sin (cos ) sin cos sin(cos ) (cos )
d dP P
d d
For l=1, m =1
The Spherical Harmonics
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18_05fig_PChem.jpg
The Spherical Harmonics
0 221
(cos( )) 3cos ( ) 12
P
1
2 (cos( )) 3sin( )cos ( )P 2 22 (cos( )) 3sin ( )P
2
2,0
5( , ) (3cos ( ) 1)
4Y f
2, 1
15( , ) sin cos
2 2
iY e f f
2, 1 2, 1 15sin cos cos
2 8
Y Y f
2, 1 2, 115
sin sin cos2 8
Y Y
i f
YZXZ
2 2
2, 2
15( , ) sin
4 2
iY e f f
The Spherical Harmonics Are Orthonormal
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The Spherical Harmonics Are Orthonormal
2
*
, , , , ,
0 0
sin( )l m l m l m l mY Y d d
f 2
0 0
1 1(cos ) (cos ) sin
2 2
m mm im m im
l l l l C P e C P e d d
f f f
2
0 0
1(cos ) (cos ) sin
2
m mim im m m
l l l l e e d C P C P d
f f f
2
,
0
(cos ) (cos ) sin2
m mm ml l
m m l l
C CP P d
2
,
0
When (cos ) (cos ) sin2
m mm ml l
l l l l
C Cm m P P d
Example0
1 (cos( )) cos( )P 0
0 (cos( )) 1P
2 20 10 10 0 0 11 1
0 1
0 0
(cos ) (cos ) sin cos sin 02 2
C CC CP P d d
Y are Eigenfuncions of H L2 L
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Yl,m are Eigenfuncions of H, L , Lz
,
1( , ) (cos( ))
2
mm im
l m l l Y C P ef f
2 2
2 2
1 1 sin
2 sin sin
d d dH
I d d d
f
22 2
2 2
1 1 sin
sin sin
d d dL
d d d
f
z
dL i
df
2
, , ( , ) ( 1) ( , )
2l m l mHY l l Y
I f f
2 2
, , ( , ) ( 1) ( , )l m l mL Y l l Y f f
, , ( , ) ( , )z l m l mL Y m Y f f
2
( 1)2
lE l lI
2 2 ( 1)lL l l
( 1)lL l l
zL m
Dirac Notation
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Dirac Notation
*
,i j i j
Sds
*
,i j i j v v
,
N
i i m m
mc f
mfis complete*
,m m m m
Sf f
* * * *
,1 ,2 , 1 ,i i i i N i N c c c c v
,1
,2
, 1
,
j
j
j
j N
j N
c
c
cc
v
Continuous Functions
Vectors
*
,|i j i j i jS
ds i i vDirac
j j v
* i j i j i j
S
ds O O O O
Bra
Ket
|j j j
H E
Dirac Notation
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Dirac Notation
2
*
1,1 1,1 1,1 1,1
0 0
( , ) ( , )sin | |H Y HY d d Y H Y
f f f 1,1 1,1
|Y HY
2 2 2
1,1 1,1 1,1 1,1 1,1 1(1 1) |
2HY Y Y Y Y
I I I
2 2
1,1 1,1|Y YI I
2
, , ( , ) ( 1) ( , )
2
l m l mHY l l Y
I
f f
2
1,1 1,1 1,0 1,0 1, 1 1, 1 | | | | | |Y H Y Y H Y Y H Y
I
Degenerate
Dirac Notation
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Dirac Notation
2
2 * 2 2
1,1 1,1 1,1 1,10 0
( , ) ( , )sin | |L Y L Y d d Y L Y
f f f 21,1 1,1
|Y L Y
2 2 2 2
1,1 1,1 1,1 1,1 1,1 1(1 1) 2 | 2L Y Y Y Y Y
2 2
1,1 1,12 | 2Y Y
2 2
, , ( , ) ( 1) ( , )l m l mL Y l l Y f f
2L
2 2
1, 1 1, 1| 2Y L Y
2
2, 1 1, 1| ?Y L Y
2 2
2, 1 2, 1| 2Y L Y
Dirac Notation
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Dirac Notation
2
*
1,1 1,1 1,1 1,1
0 0
( , ) ( , )sin | |z z zL Y L Y d d Y L Y
f f f 1,1 1,1
| zY L Y
1,1 1,1 1,1 1,1 |zL Y Y Y Y
, , ( , ) ( , )z l m l mL Y m Y f f
1,1 1,1|Y Y
1,0 1,0| | 0zY L Y 1, 1 1, 1
| |zY L Y 1,0 1,1| | ?zY L Y
3-D Rotational motion & The Angular Momentum Vector
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18_16fig_PChem.jpg
3 D Rotational motion & The Angular Momentum Vector
zL m
( 1)l l L
m indicates the orientation ofthe angular momentum with
respect to z-axis
L
l determines the length
of the angularmomentum vector
Rotational motion is quantized not continuous. Only certain
states of motion are allowed that are determined by quantum
numbers l and m.
Three Dimensional Rigid Rotor States
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Three-Dimensional Rigid Rotor States
lz mLlE,..,
l
m mY
33,2,1,0, 1, 2, 3Y
2
2,1,0, 1, 2Y
1
1,0, 1Y
2
I
6.0
3.0
1.0
0.5
0
3
2
10
Only 2 quantum numbers are require to determine the state of the system.
2
( 1)
2lE l l
I
( 1)lL l l zL m
12
6
2
Lm
0
1 0 -10
0Y
1 0-1 -2
2
1 0-1 -22
-3
3
0
2
0
2
32
0
22
Rotational Spectroscopy
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19_01tbl_PChem.jpg
Rotational Spectroscopy
Rotational Spectroscopy
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19_13fig_PChem.jpg
Rotational Spectroscopy
2
2( 1)
2J
o
E J J
r
1J JE E ED
2
1E JI
D
J : Rotational quantum number
2
2( 1)( 2) ( 1)
2o
J J J Jr
2
( 1)2J
E J JI
Rotational Spectroscopy
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Rotational Spectroscopy
hcE h hc
D
2
( 1)
4
h J
Ic
2 ( 1)B J
2 28 o
hB
r c
Wavenumber (cm-1)
Rotational Constant
1J Jv c c D D
2 ( 1 1) 2 ( 1) 2c B J B J cB
Frequency (v)
Dvv
Line spacing
Rotational Spectroscopy
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Rotational Spectroscopy
8 1 122 2 (2.99 10 / ) (1890 ) 1.13 10v cB m s m Hz D
Predict the linespacing for the 16O1H radical.
mO = 15.994 amu = 2.656 x 10-26 kg
mH = 1.008 amu = 1.673 x 10-26 kg
r = 0.97 A = 9.7 x 10-11 m
1 amu = 1 g/mol = (0.001 kg/mol)/6.022 x 10-23 mol-1
= 1.661 x 10-23 kg
27
26 27
1 1 11.774 10
2.656 10 1.673 10kg
kg kg
2 28o
hB
r c
34 21
22 27 11 8
6.626 10 /1890
8 1.774 10 9.7 10 (2.99 10 / )
kgm sm
kg m m s
1 1 12 2 (1890 ) 3780 37.8v B m m cm D
Rotational Spectroscopy
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Rotational SpectroscopyThe line spacing for1H35Cl is 21.19 cm-1,
determine its bond length .
mCl = 34.698 amu = 5.807 x 10-26 kg
mH = 1.008 amu = 1.673 x 10-26 kg
27
26 27
1 1 11.626 10
5.807 10 1.673 10
kg
kg kg
2 2 28 8o
o
h hB rr c B c
34 210
1 2 27 8
6.626 10 /1.257 10 1.257
(1059.5 )8 1.626 10 (2.99 10 / )
kgm sm A
m kg m s
11(21.19 )(100 / ) 1059.5
2 2
v cm cm mB m
D
The Transverse Components of Angular Momentum
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x
y
z
d dL i y z
dz dy
d dL i z x
dx dz
d dL i x ydy dx
zL m
( 1)l l L
L
2 2 2 2 L x y zL L L
?
?
, ( , )l mY f
zL m
2 ( 1)L l l
x y zi L L L L r i j k
The Transverse Components of Angular Momentum
Ylm are eigenfunctions ofL2 and Lz but not ofLx and Ly
Therefore Lx and Ly do not commute with either L2 or Lz!!!
Commutation of Angular Momentum Components
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g p
,x y x y y xL L L L L L
d d d d d d d d d d d d y z z x y z y x z z z x
dz dy dx dz dz dx dz dz dy dx dy dz
22
2
d d d d d y yz yx z zx
dx dzdx dz dydx dydz
2 d d d d d d d d y z z x z x y zdz dy dx dz dx dz dz dy
dz d d d d d d d d d y z yx zz zx
dz dx dz dx dz dz dy dx dy dz
product rule
Commutation of Angular Momentum Components
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g p
d d d d d d d d d d d d z x y z z y z z x y x z
dx dz dz dy dx dz dx dy dz dz dz dy
22
2
d d d d d zy z xy x xz
dxdz dxdy dz dy dzdy
d d d d d d dz d d d
zy zz xy x zdx dz dx dy dz dz dz dy dz dy
product rule
Commutation of Angular Momentum Components
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g p
22
2
22
2
2
,x y
d d d d d y yz yx z zx
dx dzdx dz dydx dydz L L
d d d d d zy z xy x xz
dxdz dxdy dz dy dzdy
z
d di ih x y i L
dy dx
,y x y x x y zL L L L L L i L
2 d d d d y x i ih y xdx dy dx dy
Commutation of Angular Momentum Components
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Commutation of Angular Momentum Components
2 x
d d d d d d d d
z x y z y z z x i Ldx dz dz dy dz dy dx dz
,x z x z z xL L L L L L
2 y
d d d d d d d d y z x y x y y z i L
dz dy dy dx dy dx dz dy
,z x z x x z yL L L L L L i L
,y z y z z yL L L L L L
,z y z y y z xL L L L L L i L
Cyclic Commutation of Angular Momentum
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Cyclic Commutation of Angular Momentum
,z x yL L i L
,y z xL L i L
,x y zL L i L
,z y x
L L i L ,
x z yL L i L ,y x zL L i L
,x y zL L i L
,y x zL L i L
xL
yL
zL
i
xL
yL
zL
i
Commutation with Total Angular Momentum
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Commutation with Total Angular Momentum
2 2 2 2 , , , ,z x z y z z zL L L L L L L L
2 2 2 ,x z x z z xL L L L L L
, , ,x z x z z x x z x z z x z x x z x zL L L L L L L L L L L L L L L L L L
, ,x x z z x x z x z xL L L L L L L L L L
x x z z x xL L L L L L
, ,x x z x z x x z x x z xL L L L L L L L L L L L
x y y xi L L i L L
Commutation with Total Angular Momentum
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g
2 2 2 ,y z y z z yL L L L L L
, ,y y z y z y y z y y z yL L L L L L L L L L L L
, ,y y z z y y z y z yL L L L L L L L L L
, , ,y z y z z y y z x z z y z y z y x zL L L L L L L L L L L L L L L L L L
y x x yi L L i L L
y y z z y yL L L L L L
Commutation with Total Angular Momentum
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g
2 2 2 2 , , , ,z x z y z z zL L L L L L L L
2 2 2 ,z z z z z zL L L L L L
0z z z z z zL L L L L L
0 0x y y x y x x yi L L i L L i L L i L L
2 , 0xL L 2 , 0yL L
This means that only
any one component of
angular momentum
can be determined at
one time.
Ladder Operators
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p
x yL L iL
x yL L iL
2 y xi L i L y xi L L
, , ,z z x z y
L L L L i L L
x yL iL L
, , ,z z x z yL L L L i L L
x yL iL L
y xi L L
( )y xi L i i L
Ladder Operators
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p
What do these ladder operators actually do???
, , ,
l m x l m y l mL Y L Y iL Y
? ?Recall That: ,zL L L
z zL L L L L
, ,
l m z z l mL Y L L L L Y
, , , ,
z l m z l m z l m l mL L Y L L Y L L Y m L Y
, , ,
l m z l m l mL Y L L Y m L Y
, ,
( 1)z l m l mL L Y m L Y
, 1 , 1 , , 1 ( 1)
z l m l m l m l mL Y m Y L Y Y Raising Operator
Lowering Operator, , 1
l m l mL Y Y Similarly
Ladder Operators
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Therefore is an eigenfunction of with eigen values land m+1
p
2 2 2 , , , 0 0 0x yL L L L i L L i 2 2 2 , , , 0x yL L L L i L L
2 2 2
, , 0 , l m l mL L Y L L L L Y
2 2
, ,
l m l mL L Y L L Y
2 2
, , ( 1)l m l mL L Y l l L Y
2 2
, ,
( 1)l m l mL L Y l l L Y
,
l mL Y2 & zL L
Which implies that, , , 1
l m l m l mL Y C Y
Ladder Operators
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p
, , , 1
l m l m l mL Y C Y
, , , 1 l m l m l mL Y C Y
This is not an eigen relationship!!!! ,l mC
is not an normalization constant!!!These relationships indicates that a change in state, by Dm=+/-1, is caused by L+and L-
Can these operators be applied indefinitely??
Remember that there is a max and min value for m, as
it represents a component ofL, and therefore must be
smaller than L. ie.
( 1) ( 1) ( 1)m l l l l m l l
2,0 2,1L Y Y
Why is lL
2,1 2,2L Y Y
2,2 0L Y Not allowed
?
, ?
n
l mL Y ,
?n
l mL Y
2,0 2, 1L Y Y
2, 1 2, 2L Y Y
2, 2 0L Y
More Useful Properties of Ladder Operators
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p p
2 2 2 2 x y zL L L L
2 2 2 2 x y zL L L L
2 2 2 2, , x y l m z l mL L Y L L Y
2 2
, ,
l m z l mL Y L Y
2
,( 1) l ml l m Y
This is an eigen equation of a physical observable that is always greater than zero,
as it represents the difference between the magnitude ofL and the square of its
smaller z-component, which are both positive.
2( 1) 0 ( 1) ( 1)l l m l l m l l
This means that m is constrained by l, and since m can be changed by1
, 1, 2,...., 2, 1, .m l l l l l l
More Useful Properties of Ladder Operators
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max, 0l mL Y
p p
min, 0l mL Y
max, 0l mL L Y min,
0l mL L Y
Lets show that mmin and mmax are land -lresp.
&L L L L Have to be determined in terms of2
& zL L
2 2 2 2 zL L L L L L
2 2 x y x y x x y y x yL L L iL L iL L iL L iL L L
2 2 x y x y x x y y x yL L L iL L iL L iL L iL L L
2 21 2
x yL L L L L L
More Useful Properties of Ladder Operators
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, , ,x yL L L L i L L
, , , ( ) ,x x y x x y y yL L i L L i L L i i L L
0 ( ) ( ) 0 2z z zi i L i i L L
Also note that:
2 2 , 2 2 zL L L L L L L L
2 2 z zL L L L L
2 2 z zL L L L L
2 2 2 2 zL L L L L L
2 2 2 2 2 2z zL L L L L
Similarly
Ladder Operators
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2 2
,max ,max 0 l z z l L L Y L L L Y
max max max
2 2
, , ,
l m z l m z l mL Y L Y L Y
max max max2 2 2
, max , max ,1 l m l m l ml l Y m Y m Y
2 max max ,1 ( 1) l ml l m m Y
max max1 ( 1) 0l l m m
maxm l
Ladder Operators
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min min
2 2
, , 0 l m z z l mL L Y L L L Y
min min min
2 2
, , ,
l m z l m z l mL Y L Y L Y
min min min
2 2 2
, min , min ,1 l m l m l ml l Y m Y m Y
min
2
min min ,1 ( 1) l ml l m m Y
min min1 ( 1) 0l l m m
2min min min1 0 1,&m m l l m l l
Since the minimum value cannot be larger than the maximum value, therefore .