Scaling Laws of Wake-Fields in Optical Structures Scaling Laws of Wake-Fields in Optical Structures Samer Banna Supervised by: Prof. L. Schächter & Prof. D. Schieber Technion – Israel Institute of Technology Department of Electrical Engineering
Scaling Laws of Wake-Fields in Optical Structures
Scaling Laws of Wake-Fields in Optical Structures
Samer BannaSupervised by:
Prof. L. Schächter & Prof. D. Schieber
Technion – Israel Institute of TechnologyDepartment of Electrical Engineering
2
OutlineOutlineOutlineBackground & Motivation
Optical AcceleratorsWake-Fields
Assumptions & approach to solutionWake-field in the vicinity of dielectric body
Radiated energyFrequency dependence of dielectric coefficient
Wake-field due to geometric discontinuityFrequency-domain versus time-domain solutionRadiated energy
Wake-field due to surface roughnessSimple model: quasi-periodic structure with random perturbationRadiated energy: average value and standard-deviation
Summary
3
Background: AcceleratorBackground: AcceleratorBackground: Accelerator
Foundation of nature (constituents of matter)
Particle physics
X – ray sources
Medical Diagnostics and treatment
Applications:
Fermilab AcceleratorAccelerator: A device used to produce high-energy (high-speed) particles by converting EM energy into kinetic energy.
4
Background: Beam-Wave InteractionBackground: BeamBackground: Beam--Wave InteractionWave Interaction
e-beam
EM-Wave EM-Wave
e-beam
1I 2 1I I<
1β 2 1β β>
Interaction
The EM wave’s phase velocity
The electrons’average velocity=
5
Motivation: Optical AcceleratorsMotivation: Optical AcceleratorsMotivation: Optical Accelerators
Cost consideration
2E Pω∝High-energy requirement
Compact accelerators based on optical structures
CompactnessHigh
frequencyHigh-gradient
6
Motivation: Lawson-Woodward TheoremMotivation: LawsonMotivation: Lawson--Woodward TheoremWoodward Theorem
No net energy gain in vacuum using optical fields
Infinite interaction region.
No walls or boundaries are present.
Highly relativistic electron on the acceleration path.
No static electric or magnetic fields present.
Non-linear effects are neglected.
7
Motivation: Lawson-Woodward TheoremMotivation: LawsonMotivation: Lawson--Woodward TheoremWoodward Theorem
Acceleration: interaction should be limited in space or time
Lawson-Woodwardtheorem conditions
No acceleration in vacuum Optical
acceleration structures
8
Motivation: Wake-FieldsMotivation: WakeMotivation: Wake--FieldsFields
Optical Acceleration Structures: Laser acceleration of electrons in vacuum entails relativistic motion of electrons in the vicinity of metallic or dielectric structures of sub-micron size.
It is important to determine:Characteristics of the wake-field.The impact of the wake-field on the bunch properties.Impact of radius of curvature.Wake-field of bunches moving/leaving geometric discontinuities.
Wake-field due to surface roughness in optical structures.Temperature consideration.Nonlinear effects.
9
Motivation: Wake-FieldsMotivation: WakeMotivation: Wake--FieldsFields
Deceleration Force
WakeWake--FieldFieldBeam Characteristics Bunch Stability
Transverse Force
10
Motivation: Wake-FieldsMotivation: WakeMotivation: Wake--FieldsFields
We focus on an analytic or quasi-analytic solutions, in order to have better understanding of the wake-field properties.
A bunch moving in a free space generates a broad spectrum of evanescent waves.
In the presence of an obstacle the evanescent waves are diffracted, carrying away energy.
11
AssumptionsAssumptionsAssumptions
An external force is acting on the moving bunch keeping its velocity constant.
Transverse motion of the moving bunch is neglected.
12
Approach to SolutionApproach to SolutionApproach to Solution
A moving bunch generates a current
density J
Excites the magnetic vector
potential A Effect of
an obstacle
A(p) - Primary fieldnon-homogeneous
wave equation
A(s) - Secondary fieldhomogeneous
wave equation
Boundary conditionsNo obstacle
13
Line Charge Moving in the Vicinity of a Dielectric CylinderLine Charge Moving in the Vicinity of a Dielectric CylinderLine Charge Moving in the Vicinity of a Dielectric Cylinder
h 2R
x
yFree space
Infinite cylinder
Constant velocity
( )00 , µε
14
Primary FieldPrimary FieldPrimary Field
)exp()(2
);,( xc
jhyyxJx βωδ
πλω −−−=
( ) 02 2 2
( )
exp sin sgn( )cos4
exp sgn( )4
p
pz
jE j x y h y hc
H j x y h y hc
ϕλµ ω ω ωϕ ϕπ β γ β γβ
λ ωπ β
− −= − −Γ − + − Γ
−= − −Γ − −
21 1;
1cos ; sin
c
x r y r
ωγγββ
ϕ ϕ
≡ Γ ≡−
= =
15
Secondary FieldSecondary FieldSecondary Field
(2)
( )
(2)
( )0
H ( , ; )
J
H ( , ; )
J
n ns jn
zn
n n r
n ns jn
nn r n r
A r r Rc
H r eB r r R
c
A r r Rc
E r j eB r r R
c
ϕ
ϕϕ
ω
ϕ ωω ε
ω
ϕ ω ηωε ε
∞
=−∞
∞
=−∞
> = <
> = <
∑
∑
0 0 0η µ ε≡
16
Longitudinal Impedance - SpectrumLongitudinal Impedance Longitudinal Impedance -- SpectrumSpectrum
||dW Zd
=Ω
20
//
zWWλ πε
∆=
||0
|| 21 Z
hZ
η≡
||
2
||
1 ( , ; ) exp( )
/ ( , ; ) exp( ) 2
1 2
x
z x
z
Z dx E x h j xc
W d dx E x h j xc
dW Zd
ωωλ β
λ ωω ωπ β
λω π
∞
−∞
∞ ∞
−∞ −∞
= −
∆ = −
⇒ =∆
∫
∫ ∫
⇒h
cω
=Ω
17
Longitudinal Impedance - SpectrumLongitudinal Impedance Longitudinal Impedance -- SpectrumSpectrum
0.0
0.5
1.0
1.5
2.0
0 25 50 75 100
Z ||
Ω
γβ =1000ε = 2r
R/h = 0.9R/h = 0.5
( ), peakpeak ZΩ
0.0
0.2
0.4
0.6
0.8
1.0
0 25 50 75 100Z ||
Ω
R/h = 0.5ε = 2r
γβ = 150γβ = 60γβ = 30
hcω
=Ωhcω
=Ω
||0
|| 21 Z
hZ
η≡
18
Longitudinal Impedance - SpectrumLongitudinal Impedance Longitudinal Impedance -- SpectrumSpectrum
Scaling Laws
peakRZh
∝ ( )1/3peakZ γβ∝ peak
hR
Ω ∝
Ω∝
1||Z
1R hΩ >>
19
Radiated EnergyRadiated EnergyRadiated Energy
Ω
Ω−
Ω
Ω
Ω−
Ω
=Ω
ΩΩ
=Ω
ΩΩ
Ω=
Ω−
∞
−∞=
∞
−∞=
∞
∑∑∫
hRJ
hRH
hRJ
hRH
ehRJU
hRJ
jV
A
AdWdAdW
rnnrrnn
rnnrnrn
n
nn
nn
εεε
εεεβ
γβ
)2()2(
22
0
)(
)(1)(1
Analytic Functions
112/
2/
)1(21)1(
21;
11
+−− −++=
Ω
−+
= nnnjn
n
n
n UjUjVehRJU
γγγγ π
20
Radiated EnergyRadiated Energy
0
10
20
30
40
50
0 500 1000 1500 2000
W
γ−1
R/h = 0.9
R/h = 0.5
R/h = 0.3
ε = 2rε = 10r
2 250γ< < 1000γ >
2
2
2 hbR RW a eh
− ≈
11.5 2a< <
10.05 0.15b< <17 10a< <
3 614 10 2 10b× < < ×
20.1 / 0.9
r
R hε >
< <
[ ]1 1ln ( 1)W a b γ≈ −
5 100; 4rγ ε< < =
25 15a< <
243 10 0.3b−× < <
21
Angular Distribution of RadiationAngular Distribution of Radiation
150
120 60
30
180 0
210 330
240 300270
90
0.1
0.2
0.30.4
0.5γβ =γβ =γβ =
1.5 0.5 0.3
150
120 60
180 0
210 330
240 300270
90
200
300
500
400
100
30γβ =γβ =γβ =
1000 100 20
Low Energies High Energies
22
Transverse KickTransverse Kick
∫∞
∞−
=−∞=−∞== yyyy dtFtPtPP )()(∆
02∆∆2
∆ηλ
π
z
yy
PP ≡
2 30∆2
zPyλ η
π γ∆
≈ ×
1γ >>
0
5
10
15
20
0 20 40 60 80 100γ−1
( γ ∆
P y )
ε = 4r
R/h = 0.7
R/h = 0.5
R/h = 0.3
23
Frequency Dependence of Frequency Dependence of Frequency Dependence of rε
0.0
0.2
0.4
0.6
0.8
1.0
0 20 40 60 80 100
Z ||
Ω
R/h=0.5
ε =2r
γβ=100
Laser pulse
; ( )
1; r C
rC
εε
Ω < ΩΩ = Ω > Ω
)200(2)0( nmWW cc =≈= λλ
pulselaser 06.1 mµ100peak nmλ ≈
c0.65W ≈ Ω4rε =
/ 0.5R h =
24
Finite Size BunchFinite Size BunchFinite Size Bunch
0
2
4
6
0 10 20 30 40 50Ω
Z ||(∆x ,
∆ y )
ε =4rR/h=0.5
γβ=10
0
5
10
15
0 10 20 30 40 50Ω
Z ||(∆x ,
∆y )
/ Z||(∆
x = 0
, ∆ y=
0) ε =4rR/h=0.5
γβ=10
rεR
βc
h
x∆
y∆
( )( )( )5.0,5.1
5.1,5.1
5.1,5.0
=∆=∆
=∆=∆
=∆=∆
yx
yx
yx ( )( )( )5.0,5.1
5.1,5.1
5.1,5.0
=∆=∆
=∆=∆
=∆=∆
yx
yx
yx
/x x R∆ = ∆ /y y R∆ = ∆
25
Finite Size BunchFinite Size BunchFinite Size Bunch
rεR
βc
h
x∆
y∆
0
10
20
30
40
0.0 0.5 1.0 1.5 2.0∆
y/R
W(∆
x , ∆ y )
/ W(∆
x=0 ,
∆ y= 0) ε =4r
R/h=0.5
γβ=10
5.10.15.0
=∆
=∆
=∆
x
x
x
Radiated energy increases with the transverse width and decreases with the longitudinal length.
Radiated energy is ∆y independent for γβ >>1 and decreases dramatically with the longitudinal length for γβ >>1.
26
Electron Bunch Traversing a Geometric DiscontinuityElectron Bunch Traversing a Geometric DiscontinuityElectron Bunch Traversing a Geometric Discontinuity
22R
1RbR2
0v
Free space
Symmetric Discontinuity
Constant velocity
( )00 , µε
27
WG Discontinuity: Frequency-Domain SolutionWG Discontinuity: FrequencyWG Discontinuity: Frequency--Domain SolutionDomain Solution
Green’s Function
( ) )0','()',0'|,0(1
20
)2(∑∞
=
Γ−<=<>ν
ννντ zeRrpJzrrzrzG
( ) ( )( ) [ ]
( ) )0','(
421
')',0'|,0(
110
1
'
)1(21
21
1010
)1(
)1(
∑
∑∞
=
Γ
∞
=
−Γ−
<+
Γ
=<<
s
zss
s
zz
ss
ss
s
s
eRrpJzr
epJR
RrpJRrpJrzrzG
ρ
πHomogeneous Solution
( ) ( ) ( ) ( )222
)2(221
)1( ; cRpcRp sss ωω ν −=Γ−=Γ
22R
1RbR2
0v
' 0z <
( )( )zj
z err
qzrJ 0v2 )(
2);,( ωδ
πω −−=
Non-Homogeneous Solution
28
WG Discontinuity: Frequency-Domain SolutionWG Discontinuity: FrequencyWG Discontinuity: Frequency--Domain Solution
Er: continuity over the cross section
Hϕ: continuity across the aperture+
Bessel functions orthogonality
Matrix Formulation
0=z
Domain Solution
Boundary Conditions
( ) ( )( ) ( )[ ] )1(1)(
)1(1)(
gYZIYZIIYT
gYZIYZIR
−++=
−+=−−
−−
)1()1(
)(
)(
)0','(
)0','(
)0','(
gzrg
Tzr
Rzr
s
s
→<
→<
→<−
−
ντ
ρ
( ) ( ) ( )21
0
1121
212
1)1(
)2(
,
2
21)( RrpJRrpdrrJRpJR
RppZ
R
ssss
s ννν
νω ∫Γ
Γ=
Single Frequency
( )( )
')1(
21
21
10)1( )1(
41
21
')0','( z
ss
ss
sepJR
RrpJzrg Γ
Γ=<
π ' 0z <
Infinite size Matrices
29
WG Discontinuity: Frequency-Domain SolutionWG Discontinuity: FrequencyWG Discontinuity: Frequency--Domain SolutionDomain Solution
( ) ( )( ) [ ]
( ) )0','(
421
')',0'|,0(
120
1
'
)2(21
22
2020
)2(
)2(
∑
∑∞
=
Γ−
∞
=
−Γ−
>+
Γ
=><
ν
νν
ννν
νν
ν
ν
τ
π
z
zz
eRrpJzr
epJR
RrpJRrpJrzrzG
Homogeneous Solution
Non-Homogeneous Solution
( )( )zj
z err
qzrJ 0v2 )(
2);,( ωδ
πω −−=
22R
1RbR2
0v
' 0z >( ) )0','()',0'|,0(
120
)1(∑∞
=
Γ>=>>s
zss
seRrpJzrrzrzG ρ
Green’s Function
( ) ( ) ( ) ( )222
)2(221
)1( ; cRpcRp sss ωω ν −=Γ−=Γ
30
WG Discontinuity: Frequency-Domain SolutionWG Discontinuity: FrequencyWG Discontinuity: Frequency--Domain Solution
Er: continuity over the cross section
Hϕ: continuity across the aperture+
Bessel functions orthogonality
Matrix Formulation
0=z
Domain Solution
Boundary Conditions
Single Frequency ' 0z >
( )
( )
(2) (2)
( ', ' 0)
( ', ' 0)
( ', ' 0)
s
s
r z R
r z T
g r z gν
ρ
τ
+
+
> →
> →
> →
( ) ( ) ( )21
0
1121
212
1)1(
)2(
,
2
21)( RrpJRrpdrrJRpJR
RppZ
R
ssss
s ννν
νω ∫Γ
Γ=
( )( )
')2(
21
22
20)2( )2(
41
21
')0','( zepJR
RrpJzrg ν
νν
νν π
Γ−
Γ=>
( ) ( )( ) ( )
1( ) (2)
1( ) (2)
R I ZY I ZY g
T Y I I ZY I ZY g
−+
−+
= + −
= + + −
Infinite size Matrices
31
WG Discontinuity: Frequency-Domain SolutionWG Discontinuity: FrequencyWG Discontinuity: Frequency--Domain SolutionDomain Solution
Single Frequency
Solution
Infinite size matrix inversion
Truncation Problems
Pulse Approaching
The DiscontinuityWide
Spectrum
Time-domain solution is preferable
Linear independent function+
Infinite size matrix inversion for each
frequency
Scalar solution
without truncation problem
Bessel function orthogonality
32
WG Discontinuity: Time-Domain SolutionWG Discontinuity: TimeWG Discontinuity: Time--Domain SolutionDomain Solution
22R
1RbR2
0v
,10
,20
Ωv
,1 011( )
Ωv
,2 021
; 0, 0
( , ; )
; 0, 0
s
zt
s ssp
zzt
rJ p e t zR
A r z t
rJ p e t zR
ν
ν νν
α
α
− −∞
=
− −∞
=
< < =
> >
∑
∑
Primary Field
( ) ( )2
, , 2 20 , 1
02
1Ω ;2 Ω
v1 ; ; , ; 1, 21
ii j i j
j j i j i
p c qR R J p
i s jc
γβ α γβπε
γ β νβ
−= =
= = = =−
33
tse 1,Ω
Long.-dependence
>
<
+
−
0 ;
0;2
1
2
2
01, v
Ω
ze
ze
Rp
Rpz
z
s
s
γβν
>
<
0;
0;
20
10
zR
rpJ
zR
rpJ s
ν
22R
1RbR2
0vFormulation: Secondary Field t<0Formulation: Secondary Field t<0Formulation: Secondary Field t<0
Metallic
BoundariesRadial-dependence
Primary Field
01, v
Ω
zts
e−− Time-dependence
34
02, v
Ω
zt
e−− ν Time-dependence
Metallic
Boundaries Long.-dependence
22R
1RbR2
0v
te 2,Ων−
,20
2 2
1 2
Ωv ; 0
; 0s
z
p pzR R
e z
e z
ν
νγβ
−
+
>
<
>
<
0;
0;
20
10
zR
rpJ
zR
rpJ s
ν
Formulation: Secondary Field t>0Formulation: Secondary Field t>0Formulation: Secondary Field t>0
Radial-dependence
Primary Field
35
>
<
=<
∑
∑
∞
=
+
−
∞
=
1,
Ω
20,
1
ΩΩ
10
)(
0;
0;
)0;,( 2
1
2
21,
01,
1,
ν
γβ
νν
ν
τ
ρ
s
Rp
Rpz
ts
s
vz
tss
sz
zeeRrpJ
z eeRrpJ
tzrAs
s
ss
22R
1RbR2
0vSecondary FieldSecondary FieldSecondary Field
>
<
=>
∑
∑∞
=
−−
∞
=
+
−
1
ΩΩ
20
1,
Ω
10,
)(
0;
0;)0;,(
02,
2,
2
2
2
12,
νν
ν
γβ
ν
νν
ν
ν
τ
ρ
z eeRrpJ
z eeRrpJ
tzrAvz
ts
s
Rp
Rpz
tss
sz
s
36
∞<<= tz 0;0Er : continuity over the cross section
Hϕ : continuity across the aperture
22R
1RbR2
0vBoundary ConditionsBoundary ConditionsBoundary Conditions
0;0 <<∞−= tzEr : continuity over the cross section
Hϕ : continuity across the aperture
are determinedss ρτ ν & ,
are determinedνν τρ & ,s
te 2,Ων−
Linearly independent
functions
tse 1,Ω
Linearly independent
functions
( )RrpJ s /0
Orthogonal set of
functions
37
22R
1RbR2
0vMagnetic FieldMagnetic FieldMagnetic Field
-1.4
-1.2
-1
-0.8
-0.6
-0.4
-0.2
2 12, 0.5 , 0bR R Rγ = = =
10.25Rtc
=−cRt 125.0=
38
Finite Size EffectFinite Size EffectFinite Size Effect
z∆
bR
( ) ( )|v|222v);,( 02
0 tzUrRUR
qtzrJ zbb
z −−∆−−=π
0 0( )
1 0U
ξξ
ξ≤
= >
0
0
0
0
1. 0;2v
2. 0;2v
3. 0;2v
4. 0;2v
z
z
z
z
z t
z t
z t
z t
∆< < −
∆< <
∆> >
∆> <
22R
1RbR2
0vz∆
39
-30
-25
-20
-15
0.2 0.4 0.6 0.8 1.0
[W(∆
z ) / W
(∆z=
0)] d
B
R2
γ = 100
∆ = 2.0z
Rb= 0.10, 0.15
Rb= 0.10, 0.15
Rb= 0.10, 0.15
∆ = 0.7z
∆ = 0.3z
-40
-30
-20
-10
0.0 0.1 0.2 0.3 0.4 0.5
[W(∆
z) / W
(∆z=
0)] d
B
Rb
γ = 100R
2 = 0.5
∆ = 0.7z
∆ = 0.3
zz
∆ = 2.0z
∆ = 5.0z
WR
qW1
10
2
2
−
≡
πε
22R
1RbR2
0vz∆
1/z z R∆ = ∆1/b bR R R=
2 2 1/R R R=
Radiated EnergyRadiated EnergyRadiated Energy
40
Radiated Energy22R
1RbR2
0vz∆
WR
qW1
10
2
2
−
≡
πε
1/z z R∆ = ∆1/b bR R R=
2 2 1/R R R=
-30
-20
-10
0
0 50 100 150 200 250
[W(∆
z ) / W
(∆z=
0)] d
B
γ−1
∆ = 2.0 = 1.0 = 0.5 = 0.3
zR
b= 0.1
R2= 0.5
0.95
0.96
0.97
0.98
0.99
1.00
0
0.01
0.02
0.03
0.04
0 50 100 150 200 250
WL /
W
WR / W
γ−1
R2 = 0.5 ∆
= 0.3zR
b = 0.3
Rb = 0.1
Rb = 0.1
Rb = 0.3
Radiated EnergyRadiated Energy
41
22R
1RbR2
0vz∆Radiated EnergyRadiated EnergyRadiated Energy
( ) [ ]25.01
212
38.01 )/(cosh
/1/11
RRR
RRW
zb ∆−
≈γγ
WR
qW1
10
2
2
−
≡
πε
1
12
1. 02. 03. 10
b
RzR R R
γ
≤ ∆ <
< < <
>
2 1
1. 0 Point Charge2. 0 Uniform Waveguide3. 0 Ultra-Relativistic
bR WR R W
Wγ
→ ⇒ → ∞
→ ⇒ →
→ ∞ ⇒ →
42
-50
-40
-30
-20
-10
0
0 50 100 150 200 250
[W] d
B
γ−1
R2= 0.5∆ = 0.5z
Rb= 0.1
ExactApproximate
-60
-50
-40
-30
-20
-10
0
0 1 2 3 4 5
[W] d
B
∆
R2= 0.5γ = 100
Rb= 0.1
Exact
Approximate
z
22R
1RbR2
0vz∆Exact vs. ApproximateExact vs. ApproximateExact vs. Approximate
43
WG Discontinuity: Time-Domain SolutionWG Discontinuity: TimeWG Discontinuity: Time--Domain SolutionDomain Solution
Time-domain analytic solution of the evanescent field in the region of the discontinuity. The solution uses the orthogonality of the Bessel functions and the fact that exponential functions describing the temporal behavior are linearly independent.Simulations based on this formulation enabled the development of an analyticexpression for the energy required to maintain the velocity of the bunch constant.
22R
1RbR2
0v
44
Surface Roughness: MotivationSurface Roughness: MotivationSurface Roughness: Motivation
?1accuracy A≈
Optical1 mλ µ≈1cmλ ≈
1accuracy mµ≈
X-band
Superposition of plane waves.Broad frequency spectrum.An assumption of small
perturbation is not necessarily relevant.
DimensionsConstrains Source Properties
Atomic level engineering.
The size of the bunch as well as the roughness of the structure are anticipated to be of the same order of magnitude.
45
v0
Roughness parameter
Partial reflection
Total charge Q
ConfigurationConfigurationConfiguration
Unif 0,ng δ ∼
in
ext, 11ext, 1 1
int intt
1 ; ; 0;2 2n n
n n n nn nn n n
R d d dzR d z z zg
Rg g
R R+
+≡ = + ≡ = ≡ = = + + +
46
Wake-Field WakeWake--Field Field
( ) ( )sinsinc
ξξ
ξ≡Current Density
( )( )
( ) 02 2
0
2 1, ;22
vsincv
zj
z b zb
QJ r z U R r eR
ωωωπ
− = − − ∆
( )1; 00; 0
U
ζζ
ζ>
≡ ≤Magnetic Vector Potential
( ) ( )2
20, ; , ;z zA r z J r z
cω ω µ ω
∇ + = −
47
Wake-Field WakeWake--Field Field
intr R<
( ) ( ) ( ) ( ) ( )0 00
, | ', ', ; 2 ' ' ' ', ';
homogeneous solutionNon-homogeneous solution
IbR
jkzz zG r z rA r z dr r dz J r z dkAz k e rω πµ ω
∞ ∞−
−∞ −∞
= + Γ∫ ∫ ∫
( ) ( ) ( )'' ', || ', jk z zkG r z r d rez gk r
∞− −
−∞
= ∫
22 2k
cω Γ ≡ −
( )( )
( ) ( )( ) ( )
0 02
0 0
' ; 0 '1' ; '2
| 'I K
K Ik
r r r r
r rr
rg r
rπ
Γ Γ ≤ ≤= Γ Γ ≤ < ∞
Green’s function in a boundless space
48
Wake-Field WakeWake--Field Field
( )( )
( )10 2
0 0
21 122
Isinc
v vz
uQ k
uB k ω ωµ δ
π
= − ∆ −
( ) ( ) ( ) ( ) ( )0 0, ; I K jkzz b BA r R z dk A k kr r eω
∞−
−∞
> = Γ + Γ ∫
( ) ( ) 0,, ; T nnz nA r z r
cDω ω ω=
0vbu Rω
γ≡
intbR r R< <
nth groove
0 0 , 00 ,, 0ext extT J Y Y Inn nr R r Rc cc c
rc
ω ω ωω ω ≡ −
Single mode
approximation
49
Wake-Field : Continuity of Ez & HϕWakeWake--Field : Continuity of Field : Continuity of EEzz & & HHϕϕ
intRcω
Ω ≡
intR∆ ≡ Γ
( ) ( ) ( ) ( ) ( ) ( ) ( )( )
20
0.21 00
12
KT
II
N
z n nn
nDA k k B kπ
ω=
∆Ω= − Ω ℑ −
∆∆ ∆ ∑
( ) ( ) ( ),1
n m nm
m
N
D Sωτ ω ω=
=∑
( ) 1sinc
2n n
njkzk e kd ℑ =
( ) ( ) ( )*
0
1 1I
n nS dk B k k∞
−∞
= ℑΩ ∆∫
( ) ( ) ( ), 1, , 0, ,T Tn m n n m m n mτ ω δ χ≡ Ω − Ω
( ) ( ) ( )1, 1 0 , 1 0 ,ext extT J Y Y In n nR Rc cω ω Ω ≡ Ω − Ω
50
Power & EnergyPower & EnergyPower & Energy
Emitted Power
( ) ( )( )
0
( ) 2 , ; , ;bR
sz zP t rdr dzJ r z t E r z tπ
∞
−∞
= ∫ ∫
Secondary field due to metallic surface
Emitted Energy
( )2 2
0 int 0 int0
( ) Re4 4
Q QW dt P t d S W
R Rπε πε
∞ ∞
−∞
≡ = Ω Ω ≡
∫ ∫
Normalized spectrum
51
v0
int0.5bR R=
int int0.15 0.3zR R< ∆ <
Typical DimensionsTypical DimensionsTypical Dimensions
int 0.5 0 0.2R mµ δ≈ ⇒ ≤ ≤30 45 1 mµ÷ ≈Bunch:
Each data point is a result ofaveraging over 80 different distributions
for a given value of δ
52
Partial Reflection in GroovesPartial Reflection in GroovesPartial Reflection in Grooves
0.0
0.3
0.5
0.8
1.0
0 0.2 0.4 0.6 0.8
W /
N
|ZL|
∆z = 0.15
∆z = 0.20
∆z = 0.25
Rb= 0.5
δ = 10-4
γ = 104
0.0
0.3
0.5
0.8
1.0
0 0.2 0.4 0.6 0.8|Z
L|
∆z = 0.15
Rb= 0.5
δ = 10-1
γ = 104
∆z = 0.20
∆z = 0.25
Grooves’number intz z R∆ ≡ ∆
- Energy almost linear with the load impedance@ .
- Energy weakly dependent on the load impedance@ .
410δ −=
110δ −=
intb bR R R≡
Normalized impedance @ grooves’ end
53
Partial Reflection in GroovesPartial Reflection in GroovesPartial Reflection in Grooves
0.0
0.1
0.3
0.4
0.5
0 10 20 30 40 50Ω
Rb = 0.5
δ = 10-1
∆z = 0.25
γ = 104
N = 10
|ZL| = 0.70
|ZL| = 0.32
|ZL| = 0.10
- Spectrum’s peak close to .- Spectrum’s width determined by
the bunch’s spectrum: sinc2 shape.
410δ −=0Ω = - Increasing the load impedance shifts
the main peak of the spectrumtowards .
110δ −=
0Ω =
0.0
0.1
0.2
0.3
0.4
0.5
0 10 20 30 40 50
|Re[
S(Ω
)]|
Ω
Rb = 0.5
δ = 10-4
∆z = 0.25
γ = 104
N = 10
|ZL| = 0.70
|ZL| = 0.32
|ZL| = 0.10
54
- The spectrum per number of grooves is virtually the same.- The total emitted energy increases linearly with the number of grooves.
1 2LZ =
0.00
0.01
0.02
0.03
0.04
0.05
0 10 20 30 40 50
|Re[
S(Ω
)]| /
N
Ω
Rb= 0.50
∆z = 0.25
δ = 0.10
γ = 104N=4,6,8,10
0
1
3
4
5
0 2 4 6 8 10
WN
Rb = 0.50
∆z = 0.25
δ = 0.10
γ = 104
Number of GroovesNumber of GroovesNumber of Grooves
55
0
Re ( )W d SΩ Ω∞
≡ ∫
0.0
0.2
0.3
0.5
0.6
0.8
0 10 20 30 40 50
|Re[
S(Ω
)]|
Ω
∆z = 0.15
∆z = 0.20
∆z = 0.25
∆z = 0.30
Rb= 0.50
δ = 0.10
γ = 104
0.0
0.2
0.3
0.5
0.6
0.8
0 10 20 30 40 50Ω
Rb= 0.50
∆z= 0.30
δ = 0.10
γ = 104
maxavg+stdavgavg-stdmin
1 2LZ =SpectrumSpectrumSpectrum
- The main peak of the spectrum isalmost independent.
- The spectrum width decreases with the increase of . z∆
z∆
- At low freq. Significant difference between average and min or max spectrum
- At high freq. all curves coincide.
56
0.0
0.2
0.3
0.5
0.6
0.8
0 10 20 30 40 50
|Re[
S(Ω
)]|
Ω
δ = 0.20δ = 0.15δ = 0.10δ = 0.05
Rb = 0.50
∆z = 0.25
γ = 103
0.0
0.2
0.3
0.5
0.6
0.8
0 10 20 30 40 50Ω
γ = 103, δ = 0.15
γ = 101, δ = 0.15
Rb = 0.50
∆z = 0.25
γ = 103, δ = 0.05
γ = 101, δ = 0.05
1 2LZ =SpectrumSpectrumSpectrum
- The spectrum is weakly dependent
on .γ- Average spectrum increases with . - Main contribution from .20Ω <
δ
57
0.0
0.2
0.4
0.6
0.8
1.0
0.00 0.04 0.08 0.12 0.16 0.20δ
Rb= 0.50
∆z = 0.25
γ > 50γ = 10
2
0 int4QW W
Rπε≡
- Average energy per groove increases with .- More energy generated by shorter bunch.- The impact of is almost negligible.
δ
γ
0.0
0.2
0.4
0.6
0.8
1.0
0.00 0.04 0.08 0.12 0.16 0.20
W /
N
δ
Rb= 0.5
γ = 104∆
z = 0.15
∆z = 0.20
∆z = 0.25
∆z = 0.30
1 2LZ =Emitted EnergyEmitted EnergyEmitted Energy
58
0.00
0.03
0.06
0.09
0.12
0.15
∆z = 0.15
∆z = 0.20
∆z = 0.25
Approx.
0.00 0.04 0.08 0.12 0.16 0.20
∆W /
δ0.25
δ
Rb= 0.5
γ = 104
- Energy spread per groove increases weakly
with average .0.25δ
22i i
i
W WW
W
−∆ ≡
0.00
0.03
0.06
0.09
0.12
0.15
γ = 101
γ = 102
γ = 103
Approx.
0.00 0.04 0.08 0.12 0.16 0.20δ
Rb = 0.50
∆z = 0.25
1 2LZ =Emitted Energy: Standard-DeviationEmitted Energy: StandardEmitted Energy: Standard--DeviationDeviation
59
Number of modes - Using a single mode is sufficient for all practical
purposes.- Use of many modes introduces numerical noise.
0.00
0.01
0.02
0.04
0.05
0.06
0 10 20 30 40 50
|Re[
S(Ω
)]| /
Ν
Ω
Rb = 0.5
∆z = 0.3
γ = 104
M = 2,3,4
M = 1
Single Mode ApproximationSingle Mode ApproximationSingle Mode Approximation
60
Summary: Scaling-LawsSummary: ScalingSummary: Scaling--Laws
22 0.25
2int int
0 int
int
int int
0.15 tanh 121.2
4
451.4290.57 tanh
1 20.72 1 20.72z z
W W g gR RQ N
R
gR
R R
πε
∆ ∆
∆ ∆
− ×
× +
+ +
int2
int int0 int
451.4290.57 tanh
1 20.72 1 20.724
z z
gW R
Q NR RRπε∆ ∆
+
+ +×
Average Energy
average roughnessLaws
roughness std.Standard Deviation
61
Summary: Scaling-LawsSummary: ScalingSummary: Scaling--LawsLaws
2
0 int
24
W QN Rπε
×
Average EnergyPoint-Charge0z∆ =
Standard Deviation
22 0.252
0 int int
0.34
W W Q gN R Rπε
− ∆×
- Point-charge moving in a cylinder of radius Rint boredin a dielectric or metallic medium
- Point-charge moving in a cylindrical wave-guide withperiodic wall of arbitrary but azimuthally symmetric geometry.