Electron-Acoustic Wave in a Plasma - Peopleattwood/sxr2009/... · Ch06_ElectrnAcoustWv2.ai...
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Ch06_ElectrnAcoustWv1.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Electron-Acoustic Wave in a Plasma
For small fluctuations, ne/n0
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Ch06_ElectrnAcoustWv2.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Electron-Acoustic Wave in a Plasma (continued)
with sound speed ae given by
and plasma frequency ωp given by
These can be combined to form a wave equation
or
Taking ∂/∂t of Eq. (6.75), of Eq. (6.76),
(6.78)
(6.79)
(6.80)
This can be rewritten as a longitudinal wave equation for electron density fluctuations
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Ch06_ElecAcousWvDispr.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Electron-Acoustic Wave: Dispersion Relation
(6.78)
(6.84)
(6.83)
For an electron density wave of the form
We have, as in chapter 2,
and
so that the wave equation takes the form
This has solutions for finite electron density ne when when the bracketedoperator is zero, giving the dispersion relation for the electron-acousticwave
For long period plasma waves, where k goes to zero, there is a natural oscillation at the electron plasma frequency, ω ωp. For waves of finite k,in the range of 0 ≤ k ≤ ωp/ae, the frequency increases somewhat, to a valueof 2 ωp at k = ωp/ae, as shown in the dispersion diagram, next page.
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Ch06_DispersionDiagrm.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Electron-Acoustic Wave: Dispersion Diagram
(6.84)
Dispersion relation:
Dispersion diagram:
ωp
ae
kD = 1/λD k
a*
cElectromagnetic wave
Electron-acousticwave
Freq
uenc
y
Wavenumber
ω
Ion-acousticwave
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Ch06_TransvrseElectro1.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Transverse Electromagnetic Waves in a Plasma
For transverse waves in a plasma, we neglect the longitudinal fieldcomponents ( → ik terms). The transverse fields are described by
Take ∂∂t of eq. (6.99) and curl of eq. (6.100) to obtain
(6.99)
(6.100)
(6.103)
(6.106)
Eliminate the ∂H/∂t terms and use the vector identity ( E) = ( E) – 2E to form
(6.104)
(6.105)
and
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Ch06_TransvrseElectro2.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Transverse Electromagnetic Waves in a Plasma(continued)
0 for transverse fields
For a plane wave of the form E(r, t) = E0e–i(ωt – kr) this yields a dispersion relation
Rearranging terms
(6.106)
(6.107)
(6.108)
Recognizing c2 = 1/0µ0 and ω2 = e2n/0m, we have the wave equation for a transverse wave in a plasma,
p
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Ch06_TransvrseElectro3.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Transverse Elecromagnetic Waves in a Plasma
(6.108)
Dispersion relation:
Dispersion diagram:
ωp
ae
kD = 1/λD k
a*
c
Electromagnetic wave
Electron-acousticwave
Freq
uenc
y
Wavenumber
ω
Ion-acousticwave
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Ch06_PropagatnOvrdns1.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Propagation in an Overdense Plasma
(6.108)
(6.109)
(6.110)
(6.111)
2
Solving for k
which corresponds to a penetration depth l into the highlyoverdense plasma of
For ω < ωp, k is imaginary, the wave exponentially decays.In the highly overdense limit ω
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Ch06_PropagatnOvrdns2.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Propagation in an Overdense Plasma (continued)
(6.108)
(6.112a)
(6.112b)
The frequency for which ω = ωp, is referred to as the cutoff or critical frequency, and corresponding electron density is defined as the critical electron density, nc
or in terms of the wavelength (in microns)
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Ch06_RefracIndxPlas.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Refractive Index of a Plasma
(6.113a)
(6.114a)
(6.114b)
For ω > ωp there is a real propagating wave with phase velocity
The refractive index of the plasma is
or equivalently
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Ch06_PhaseGroupVelo1.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Phase Velocity and Group Velocity
In a dispersive medium different frequency components travel with different phase velocities. If there is some frequency modulation, the various components will interfere to form a modulation envelope, which will travel at a different, slower velocity. The velocity with which the envelope moves is known as the “group velocity”. We associate the group velocity with information or energy transport.
Reference: E.C. Jordon, Electromagnetic Waves and Radiating Systems (Prentice-Hall, NJ, 1950).
Modulationenvelope, vg
Individual frequency components, vφ
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Ch06_PhaseGroupVelo2.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Phase Velocity and Group Velocity (continued)
Dispersion relation:
(6.108)
(6.113a)
(6.113b)
Phase velocity:
Group velocity:
where we associate group velocity with information orenergy transport. For ne/nc
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Ch06_CollisnalAbsrptnTrans.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Collisional Absorption of a Transverse Wavein a Plasma
The analysis is readily extended to include the effect of collisions betweenelectrons, oscillating due to the transverse wave, and ions. By including acollision term, the electron momentum transfer equation (6.103) becomes
(6.115)
where the momentum transfer is proportional to the electron momentum mvand where vei is the electron-ion collision frequency. The electron velocitycan be written as
and the dispersion relation (6.108) modified, for vei
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Ch06_WvsMagntzdPlas.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Waves in a Magnetized Plasma
k
ω
ωc
kD
c
ωρ
Cyclotronresonance
Plasmaresonance
Freq
uenc
y
Wavenumber
Hybridresonance
(θ = 0)
(θ = 0)
(θ = 0)
(θ = π/2)(π/2)
(π/2)
(0)
ω2 + ω2ρ c
(π/2)
(6.5)
(6.8)
(Courtesy of N. Marcuvitz.)
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Ch06_NonLinearProc.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Non-Linear Processes in a Plasma
(6.123a)
(6.123b)
(6.123c)
(6.123d)
Product terms lead to non-linear growth and frequency mixing
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Ch06_LinearNonLinScat2.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Linear and Non-Linear Processes: Scattering as an Example
Three wave mixing among natural modes of the plasma. In resonant mixing the three satisfy conservation of energy and momentum.
(6.125a)
(6.124b)
• Linear scattering
• Non-linear scattering(6.125b)
ω1, k1ω2, k2
ω3, k3
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Ch06_StimBrillouin.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Stimulated Brillouin and Raman Scattering of Intense Laser Light
ω
(ωR, kR)
(ωi, ki)
Electron-acoustic(high frequency)
(ωea, kea)
e– - w
ave
kk
ωi = ωea + ωRki = kea + kR
ωi = ωia + ωBki = kia + kB
0
ω
(ωB, kB)
(ωia, kia)
(ωi, ki)
Ion-acoustic(low frequency)
0
Electromagneticwave
EM
(a) Brillouin:
Ion-wave
(b) Raman:
ωPeωPe
By resonant three-wave mixing naturally occurring wavesare driven out of the noise, to large amplitude, by an intenseincident electromagnetic wave.
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Ch06_StimRamanBackscat.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Stimulated Raman Backscattering at ne nc/4
(ωea, kea)
k
ae
ki kea = ki + ∆kkR = ∆k
(ωi, ki)
ωp
ω ccIncident electromagnetic wave
Electron-acoustic waveScattered electromagnetic wave
(ωR, kR)
(following H. Motz)
Frequency and wavenumber matching occurs at the quarter-critical surface.For κTe = 1 keV, matching occurs at ωea = 1.005ωp, ωi = 2.005ωp, andki = 3 ωp/c. The phase velocity of the stimulated electron acoustic wave
Trapped electrons within the waves high potential crests can be acceleratedto velocities of c/ 3 , corresponding to electron energies of order 100 keV.and will radiate x-rays of order 100 keV. (Reference: Turner, Drake, Campbell, LLNL).
(6.130)
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Ch06_VeryHardXRs_IntensLasRad.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Very Hard X-Rays Can be Generatedby Intense Laser Radiation
Photon energy (ω)
Near thermalcontinuum
L-shell emission linesS
pect
ral e
mis
sion
inte
nsity
K-shell emission lines
Non-thermal radiationdue to hot or supra-thermal electrons
Typically strong non-linear mixing occurs for
where and
(6.131)
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Ch06_ContRadBlackSpec.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Continuum Radiation and BlackBody Spectra
Hot-dense plasmas with sharp spatial and temporal gradients,rapid expansion, and a variety of temperatures (Te, Ti, Thot, . . .)are not in equilibrium. Nonetheless a great fraction of the radiated energy is in a near-thermal distribution. Thus it is of value to consider the limiting case of blackbody radiation, that emitted by matter in equilibrium with its’ surroundings, and characterized by a single temperature T. Following Planck (1900), the spectral energy density U∆ω inunits of energy per unit volume, per unit frequency interval∆ω at frequency ω, is
in units of ∆2E/∆V ∆ω. In terms of relative spectral bandwidth, ∆ω/ω,
where κ is the Boltzmann constant
(6.134a)
(6.134b)
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Ch06_BlackbdyRad.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Blackbody Radiation
with peak at
(6.136a)
(6.137)
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Ch06_BlkbdyRadEqLmt.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Blackbody Radiation: The Equilibrium Limit
(6.136b)
(6.137)
(6.138b)
Example: κT = 100 eV, B∆ω/ω = 4.47 1017
1.4
1.8
1.0
0.6
0.2
0 2 4 6 8Photon energy (x)
Spe
ctra
l brig
htne
ss
x = 2.822
x =
x3(ex – 1) ω
κT
2.82 κT
photons/secmm2 mrad2 (0.1% BW)
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Ch06_BlkbdyRadSurface.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Blackbody Radiation Across a Surface
The power per unit area across a surface, in one direction, per unit spectral bandwidth, is
Integrating over all frequencies
The blackbody intensity at any interface is
where σ is the Stefan-Boltzmann constant. Written with κT expressed in electron volts
(6.143a) ; (6.143b)
Example: For κT = 100 eV, I = 1.027 1013 W/cm2.
where θ is mearsured from the surface normal, dΩ = sin θ dθ dφ = 2π sin θ, for 0 ≤ θ ≤ π/2, and where I∆ω/ω has units of energy per unit area per unit of relative spectral bandwidth ∆ω/ω. Since the spectral brightness is isotropic (no θ-dependence), and 0 2π sin θcosθdθ = π, one has
2π
(6.139)
(6.140)
(6.141)
κT
κT
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SEMATECH Sources : 3.3.2002Dr. Lebert, Dr. Juschkin , AIXUV
Planck radiator: the most brilliant radiator in nature except for a laser
Thermal PlasmaEmission:
Line radiation
Rekombinationradiation .
Bremssstrahlung
maximum Brilliancefor a given
temperature
Radiation is inequilibrium with
matter(Kirchhoff)
Thermal PlasmaEmission:
Line radiation
Rekombinationradiation .
Bremssstrahlung
maximum Brilliancefor a given
temperature
Radiation is inequilibrium with
matter(Kirchhoff)
( )BBkTISj
)(ννν
ν
α==
10-1 100 101 102 103 104
Wellenlänge [nm]
Log (
Lλ)
Bremsstrahlung
Rekombination radiation
Line radiation
Planck
ωL=ωpe
Ch06_PlanckRadiatr.ppt
Courtesy of Dr. R. Lebert
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Soft X-Ray/EUV Emission from a Laser-Produced Plasma
Ch06_F05VG.modif.ai
Distance
Laser-plasmainteraction region
Laser light
Hot dense region ofintense x-ray emission
Ele
ctro
n de
nsity
nc• κTe ~ 50 eV to 1 keV• ne ~ 1020 to 1022 e/cm3
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
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Ch03_NotchFilter.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
The Notch Filter
• Combines a glancing incidence mirror and a filter• Modest resolution, E/∆E ~ 3-5• Commonly used
Mirrorreflectivity(“low-pass”)
Absorptionedge Filter
transmission(“high-pass”)
Photon energy
1.0
Filter/reflectorwith responseE/∆E 4
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Ch06_F.24VG.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Measuring Continuum Emission from a Hot Dense Plasma
Laserirradiated
target
EUV/Soft X-rayemission
Glancingincidence
mirrors
θ
Soft X-raystreak camera
Opticaltrigger
Filter pack
Thin foil cathode substrate
Time
Courtesy of G. Stradling, R. Kauffman, and H. Medecki, LLNL.
• Cross-calibrate each channel with a fast, calibrated EUV/X-ray diode
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Ch06_F.25VG.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Determining an Equivalent Blackbody Temperature
1011
1010
109
108
1070 1000 2000
Time (ps)
Equ
ival
ent r
adia
tion
tem
pera
ture
(eV
)
3000
300
250
200
150
100
790 psec FWHM
50
Au disk2ω, 0.53 mEL = 355, τL 680 psΙ 1 × 1015 W/cm2Focal diameter 80 m
200 eV
400 eV
600 eV
Time
Rad
iate
d po
wer
per
cha
nnel
Rad
iate
d so
ft x-
ray
pow
er (W
atts
)
(Courtesy of R. Kauffman, LLNL)
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Ch06_MeasurePlasRad.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Measuring Plasma Radiationin Specific Narrow Spectral Bands
Laserirradiated
target
Soft X-rayemission
CHCFSiO2
Layeredtarget Laser
light
Multilayermirrors (5)
25°
Soft x-raystreak camera
Filters (5)
Time
0
1
10–1
10–2
1,000Time (psec)
Rec
orde
d so
ft x-
ray
sign
al (r
elat
ive)
2,000 3,000
102 eV737 eV943 eV
0.27 µm Be on A1.06 µm89J, 720 ps3 × 1014 W/cm2
(Courtesy of G. Stradling)
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Ch06_LineContinRad3.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Multiple Ionization States Result in Many Emission Lines
Photon energies for bound-boundtransitions depend on the ionization state.
+Ze
n = 3
n = 2
n = 1
10e– 9e– 8e–
ω
+Ze
ω
+Ze
ω
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Ch06_F.23VG.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Soft X-Ray Emission Spectrafrom a Laser Produced Plasma
0.80
0.75
0.70
0.65
0.60
0.55
500 550Photon energy (eV)
Film
den
sity
600 650 700 800750
Cr+14(3s - 2p)
Cr+15(3s - 2p)
Cr+14(3d - 2p) Fe L-edge(707 eV)
(Courtesy of R. Kauffman and L. Koppel, LLNL)
The dominant “neon-like” Cr+14 has 10 electrons: 1s2 2s2 2p6 (ground state)and a 1012 eV ionization energy
1.06 µm laser2 1014 W/cm2150 psecCr (Z = 24)
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Ch06-IonzBtlnecks2.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Ionization “Bottlenecks” Limit the Numberof Ionization States Present in a Plasma
Cr target at2 1014 W/cm2κTeq 200 eV4κTeq 800 eV(too low to efficiently ionize neon-like Cr+14 to Cr+15)
(Courtesy of J. Scofield, LLNL)
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Ch06_Atomic_IonicBk.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
Three volumes,bound as books
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Ch06_ChromiumChart.ai
Professor David AttwoodAST 210/EECS 213Univ. California, Berkeley
R. Kelley: Atomic and Ionic Spectral Lines
Neon-like Cr
(670 eV)(660 eV)
(594 eV)
(586 eV)