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Transcript of Internal partition function calculated with where N is the particle density (cm 3 ) Influence of...
![Page 1: Internal partition function calculated with where N is the particle density (cm 3 ) Influence of Electronically Excited States on Thermodynamic Properties.](https://reader030.fdocuments.net/reader030/viewer/2022032806/56649efe5503460f94c130c5/html5/thumbnails/1.jpg)
THERMODYNAMICS, TRANSPORT PROPERTIESAND KINETICS
OF PARTIALLY IONIZED GASES
M. Capitelli
Chemistry Department, University of Bari, ItalyIMIP-CNR, section of Bari, Italy
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kT
EN
n
n
enF−
=∑=max
1
2int 2
Internal partition function
calculated with
30
max1
Nan =
where N is the particle density (cm3)
Influence of Electronically Excited States on Thermodynamic Properties of LTE Hydrogen Plasma
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Ratio of inner enthalpy to total enthalpy at different pressure.
⎟⎠⎞
⎜⎝⎛+⎟
⎠⎞
⎜⎝⎛ +++⎟
⎠⎞
⎜⎝⎛ ++= + kTnEI
DkTn
DEkTnH eHH 2
5'
22
5'
22
5'
€
Hint = n'H E
The total enthalpy of all the system is calculated as follows:
while the inner part of enthalpy is equal to:
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⎟⎠⎞
⎜⎝⎛+⎟
⎠⎞
⎜⎝⎛+⎟
⎠⎞
⎜⎝⎛ +=⎟
⎠⎞
⎜⎝⎛∂∂
= + knkncknT
Hc eHVH
nPP
i
f 2
5'
2
5'
2
5'
int',
€
cptot=
∂H∂T
⎛
⎝ ⎜
⎞
⎠ ⎟P
=cpf+ cprthe total specific heat is diveded in two
parts:
the frozen specific heat
⎟⎠⎞
⎜⎝⎛
⎟⎠
⎞⎜⎝
⎛∂∂
+⎟⎠⎞
⎜⎝⎛ ++⎟⎟
⎠
⎞⎜⎜⎝
⎛
∂
∂+⎟
⎠⎞
⎜⎝⎛ ++⎟
⎠
⎞⎜⎝
⎛∂∂
=+
kTT
nEI
DkT
T
nDEkT
T
nc
P
e
P
H
P
HPr 2
5'
22
5'
22
5'the reactive specific heat
the inner specific heat is :
Ratio of inner Cp to total Cp at different pressure
intint ' VH cnc =
Ratio of inner Cp to Cp frozen at different pressure
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Ratio of Cp, using Debye-Huckel theory, to Cp calculated with cut-
off, at 108 Pa.
Ratio of Cp, using Debye-Huckel theory, to Cp calculated with cut-
off, at 105 Pa.
Internal specific heat and his component at 108 Pa.Internal specific heat and his component at 105 Pa.
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The transport properties of a partially ionized thermal hydrogen plasma has been calculated by taking into account electronically excited states with their “abnormal” transport cross sections. The results show a strong dependence of these
transport properties on electronically excited states specially at high pressure.
• Translational thermal conductivity • Viscosity
Heavy particles transport properties Electron transport properties
• Translational thermal conductivity
• Electrical conductivity
• Reactive thermal conductivity
“Usual” Collision integrals “Abnormal” Collision integrals
€
ΩH n( )−H + = Ω
H 1( )−H +
ΩH n( )−H m( )= ΩH 1( )−H 1( )
ΩH n( )−e = ΩH 1( )−e
Complete set of data (see text)
Influence of Electronically Excited States on Transport Properties of LTE Hydrogen Plasma
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Model
• Species
We have considered an hydrogen plasma constituted by molecular hydrogen, atomic hydrogen (12 atomic levels), H+ ions and electrons:
• H2
• H(n=1,12)• H+
• e-
• Reactionswe consider the dissociation process and ionization reactions starting from each electronic states of hydrogen atom.
€
H2 ↔ 2H1
€
H n =1,12( ) ↔ H + +e−
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Equilibrium Composition
The equilibrium composition is obtained by using Saha and Boltzmann laws. First we calculate the equilibrium composition by considering only four species and two reactions which take into account the total atomic hydrogen without distinction among the electronic states.
Then we use the Boltzmann distribution for calculating the distribution of the electronic states of atomic hydrogen.
€
NH2
NH 2
=QH
QH 2
2πmekbTh2
⎛ ⎝ ⎜
⎞ ⎠ ⎟3 2
12
⎛ ⎝ ⎜
⎞ ⎠ ⎟3 2
exp −ED
kbT
⎛
⎝ ⎜
⎞
⎠ ⎟
€
NeNH +
NH
=2 ⋅g
H +
QH
2πmekbTh2
⎛ ⎝ ⎜
⎞ ⎠ ⎟3 2
exp −E I
kbT
⎛
⎝ ⎜
⎞
⎠ ⎟
€
ni = ngi
Z T( )e−Ei kBT
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Collision Integrals I: General Aspects
Transport cross sections can be calculated as a function of gas temperature according to the equations
€
Ωij( l ,s) =
kT2πμ ij
0
+∞
∫ e−γ ij2
γ ij2s+3σ ( l ) (g)dγ ij
€
σ ( l ) (g) = 2π (1−cos l χ )bdb0
+∞
∫
where
€
γij2 =
12
μ ijg2 / KT
Considered interactions:
• neutral-neutral (H2-H2, H2-H, H-H)
• ion-neutral (H+-H2, H+-H)
• electron-neutral (e-H, e-H2)
• charged-charged (H+-e, H+-H+, e-e)
For the present calculation we need the collision integrals of different orders depending on the different approximations used in the Chapman-Enskog method. To this end we have used a recursive formula
€
Ω (l ,s +1) = TdΩ (l ,s )
dT+ s+
3
2
⎛ ⎝ ⎜
⎞ ⎠ ⎟Ω (l ,s )
Note that we have used the reduced collision integrals i.e. the collision integrals normalized to the rigid sphere model Ωij
*
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Collision Integrals II: e-H(n)
Diffusion type collision integrals for the interactions e-H(n) are calculated by integrating momentum transfer cross sections of Ignjatovic* et al..
Viscosity type collision integrals have been considered equal to diffusion type ones
€
Ωe−H n( )
2,2( )* = Ωe−H n( )
1,1( )*
*L.J. Ignjatovic, A.A. Mihajlov, Contribution to Plasma Physics 37 (1997) 309.
0.0
50.0
100.0
150.0
200.0
250.0
1.0 1.2 1.4 1.6 1.8 2.0
n'= 2 - 1/n2
Ω(1,1)∗
( Å
2 )
( )-H n e
=1n
=10n
T=104 K
T=2 104 K
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Collision Integrals III: H+-H(n)
Diffusion type and viscosity type collision integrals have been calculated by Capitelli et al.* and fitted according to the following expressions.
100
101
102
103
1.0 1.2 1.4 1.6 1.8 2.0
Ω (2,2)
(Å
2 )
n=1
n=2n=3
n=4n=5
n' = 2 - 1n2
H(n)+H
+
T =104 K
101
102
103
104
105
1.0 1.2 1.4 1.6 1.8 2.0
Ω (1,1) (Å
2 )
( )- H n H
+
′ n = 2 −
1
n
2
=1n
=2n
=3n
=4n=5n
T =104 K
€
ΩH n( )−H +ct
1,1( )* T( ) = exp f1 ′ n f2 ′ T f3 +exp f4 ′ n − f5( )( )
€
ΩH n( )−H +
2,2( )* T( ) = exp g1 ′ n g2 ′ T g3 +exp g4 ′ n − g5( )( )
with
€
′ T =T 1000
*M. Capitelli, U.T. Lamanna, J. Plasma Phys.12, 71 (1974).
The elastic contribution to Ω(1,1)* has been evaluated with a polarizability model
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Collision Integrals IV: H(n)-H(n)
Viscosity type collision integrals for the interactions H(n)-H(n) up to n=5 have been calculated by Celiberto et al.* By using potential energy curves obtained by CI (configuration interaction) method. The data have been interpolated at different temperatures with the equation
€
ΩH n( )−H n( )
2,2( )* = exp a1 +exp −a2 ′ n + a3( )( )
where
€
′ n = 2 −1n2
*R. Celiberto, U.T. Lamanna, M.Capitelli, Phys.Rev A 58, 2106 (1998).
0.0
5.0
10.0
15.0
20.0
25.0
30.0
1.0 1.2 1.4 1.6 1.8 2.0
n'
H(n)-H(n)Ω
(2,2)∗
( Å
2 )
=1n
=5n
= 2 - 1/n2
T=104 K
T=2 104 K
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Collision Integrals V: H(n)-H(m)
0.0
5.0
10.0
15.0
20.0
25.0
30.0
1.0 1.2 1.4 1.6 1.8 2.0
Ω (2,2) (Å
2 )
( )- ( )H n H m
=1n=2n
=3n=4n
=1m=2m
=3m
(1,1)
(2,2)
(3,3)
(4,4)
= 2 - n' 1n2
T =104 K
10-2
10-1
100
101
102
103
104
105
106
1.0 1.2 1.4 1.6 1.8 2.0
Ω (1,1) (Å
2 )
( )- ( )H n H m
′ n = 2 −
1
n
2
=1n
=2n=3n=4n
= +1m n
= +2m n
= +3m n
(1,2)
(2,3)(3,4)
(1,3)
(2,4)
=10T 4 KM.Capitelli, P.Celiberto, C.Gorse, A.Laricchiuta, P.Minelli, D.Pagano, Phys. Rev. E 66,016403/1 (2002)
€
ΩH n( )−H m( )
2,2( )* T( ) =12
ΩH n( )−H n( )
2,2( )* +ΩH m( )−H m( )
2,2( )*( )
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Transport Coefficients I: General Aspects
Transport coefficients have been calculated by using the third approximation of the Chapman-Enskog method for the electron component and the first non-vanishing approximation for heavy components.
In general we have considered 12 electronically excited states; at high pressure we have reduced the number of excited states to 7 to take into account the decrease of the number of the electronically excited states with increasing pressure.
Cut-off criterium
We include in the electronic partition function all the elctronic states with radius less than the average distance between particles
€
a0nmax2 =
1′ n
⎛ ⎝ ⎜
⎞ ⎠ ⎟
13
where
€
′ n =p
kBT
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Transport Coefficients II: Translational Thermal Conductivity
Heavy particles Electrons
Chapman-Enskog method
Second order approximation
€
λ trh = 4
L11 K L1v
M O M
Lv1 K Lvv
x1 K xv
x1
M
xv
0L11 L L1v
M O M
Lv1 L Lvv
Third order approximation
€
λ tre =
758
1016 nekB
2πkBTe
me
⎛
⎝ ⎜
⎞
⎠ ⎟
12 q 22
q11q 22 − q12( )
2
€
Lii = −4 x i
2
λ ii
−2x ixK
λ iK
1
M i + M j( )2
K=1K≠ i
v
∑ 1
AiK*
15
2M i
2 ⎛
⎝ ⎜ +
25
4MK
2 − 3MK2 BiK
* + 4M iMK AiK* ⎞
⎠ ⎟
€
Lij =2xjxi
λij
M iM j
M i + M j( )2
1
AiK*
55
4− 3Bij
* − 4Aij* ⎛
⎝ ⎜
⎞
⎠ ⎟
€
Aij* =
Ωij(2, 2)*
Ωij(1,1)*
€
Bij* =
5Ωij(1, 2)* − 4Ωij
(1, 3)*
Ωij(1,1)*
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Transport Coefficients III: Reactive Thermal Conductivity
For a gas constituted by chemical species and independent reactions the reactive thermal conductivity can be calculated by means of Butler and Brokaw theory
€
λR = −1
RT 2
A11 K A1μ
M O M
Aμ 1 K Aμμ
ΔH1 K ΔHμ
ΔH1
M
ΔHμ
0
A11 K K
M O M
M K K
Aμ 1 K K
A1μ
M
M
Aμμ
€
Aij =RT
DklPxK xl
aik
xk
−ail
xl
⎛
⎝ ⎜
⎞
⎠ ⎟a jk
xk
−a jl
xl
⎛
⎝ ⎜
⎞
⎠ ⎟
l=k+1
v
∑k=1
v−1
∑
where
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Transport Coefficients IV: Viscosity
Viscosity has been calculated by means of the first approximation of the Chapman-Enskog method
€
η =−
H11 K H1v
M O M
H v1 K H vv
x1 K xv
x1
M
xv
0
H11 L H1v
M O M
H v1 L H vv
The Hij are expressed as a function of temperature, collision integrals and molecular weight of the species, while i represents the molar fraction of the i-th component
€
Hij = −2xi x j
η ij
M iM j
M i + M j( )2
⎛
⎝ ⎜ ⎜
⎞
⎠ ⎟ ⎟
53Aik
*−1
⎛
⎝ ⎜
⎞
⎠ ⎟
€
Hii =xi
2
η ii
+2xi xk
η ik
M iM k
M i + M k( )2
⎛
⎝ ⎜ ⎜
⎞
⎠ ⎟ ⎟
k=1k≠i
v
∑ 53Aik
*+
M k
M i
⎛
⎝ ⎜
⎞
⎠ ⎟
€
Aij* =
Ω ij(2,2 )*
Ω ij(1,1)*
€
ηij =2.66932.628
10−2 2M iM j
M i + M j
P0Dij
Aij*T
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Transport Coefficients V: Electrical Conductivity
The electrical conductivity has been calculated by using the third approximation of the Chapman-Enskog method
€
σ =32
e2ne2 2π
meKT
⎛
⎝ ⎜
⎞
⎠ ⎟
12 q11q 22 − q12
( )2
q 00 q11q 22 − q12( )
2
( )+q 01 q12q 02 −q 01q 22( )+q 02 q 01q12 −q 02q11
( )
€
q 00 = 8ne n jQej(1,1)*
j =1
ν −1
∑
€
q 01 = 8ne n j
5
2Qej
(1,1)* − 3Qej(1,2 )* ⎛
⎝ ⎜
⎞ ⎠ ⎟
j =1
ν −1
∑
€
q 02 = 8ne n j
35
8Qej
(1,1)* −21
2Qej
(1,2 )* + 6Qej(1,3)* ⎛
⎝ ⎜
⎞ ⎠ ⎟
j =1
ν −1
∑
where
The presence of electronically excited states can affect σe through the collisions e-H(n)
€
q11 = 8 2 ne Qee(2,2 )* + 8 n j
25
4Qej
(1,1)* −15Qej(1,2 )* +12Qej
(1,3)* ⎛ ⎝ ⎜
⎞ ⎠ ⎟
j =1
v−1
∑
€
q12 = 8 2 ne
7
4Qee
(2,2 )* − 2Qee(2,3)* ⎡
⎣ ⎢ ⎤ ⎦ ⎥+ 8
j =1
v−1
∑ n j
175
16Qej
(1,1)* − ⎛ ⎝ ⎜
−315
8Qej
(1,2 )* + 57Qej(1,3)* − 30Qej
(1,4 )* ⎞ ⎠ ⎟
€
q 22 = 8 2 ne
77
16Qee
(2,2 )* − 7Qee(2,3)* + 5Qee
(2,4 )* ⎡ ⎣ ⎢
⎤ ⎦ ⎥+ 8 n j
j =1
v−1
∑ 1225
64Qej
(1,1)* ⎛ ⎝ ⎜ −
−735
8Qej
(1,2 )* +399
2Qej
(1,3)* − 210Qej(1,4 )* + 90Qej
(1,5 )* ⎞ ⎠ ⎟
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Results I: Diagonal Approximation (Viscosity)
0.0 100
2.0 10-5
4.0 10-5
6.0 10-5
8.0 10-5
1.0 10-4
0
2
4
6
8
10
1 104 1.5 104 2 104 2.5 104 3 104
Viscosity [Kg m
-1 s
-1] |η
( )b- η( ) a
|*100 /
η( )b
[ ]Temperature K
0.0 100
2.0 10-5
4.0 10-5
6.0 10-5
8.0 10-5
0
20
40
60
80
100
1 104 1.5 104 2 104 2.5 104
Viscosity [Kg m
-1 s
-1] |η
( )b- η( ) a
|*100 /
η( )b
[ ]Temperature K
The small relative error indicate a sort of compensation between diagonal and off-diagonal terms.
The differences calculated with the two sets of collision integrals are very higher.
Including off-diagonal terms
Neglecting off-diagonal terms
This point can indicate the importance of using higher Chapman - Enskog approximations for the calculation of the viscosity in the presence of excited states.
“usual” collision integrals: solid line
“abnormal” collision integrals: dashed line
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Results II: Heavy Particles Translational Thermal
Conductivity
0.00
1.00
2.00
3.00
4.00
5.00
10000 15000 20000 25000 30000
λ( )ah
[ ]Temperature K
=7n
=12n
1atm
10atm
[ W m
-1 K
-1]
100atm
0.30
0.40
0.50
0.60
0.70
0.80
0.90
1.00
10000 15000 20000 25000 30000
λ( )a / λ( )u
[ ]Temperature K
100atm
=7n
=12n
1atm
10atm
h
h
The ratio between the translational thermal conductivity values calculated with the “abnormal” cross sections (λh
a) and the corresponding results calculated with the “usual” cross sections (λh
u) is reported as a function of temperature for different pressures.
The small effect observed at 1 atm is due to the compensation effect between diagonal and off-diagonal terms in the whole representation of the translational thermal conductivity of the heavy components. This compensation disappears at high pressure as a result of the shifting of the ionization equilibrium
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Results III: Electron Translational Thermal
Conductivity
0.00
2.00
4.00
6.00
8.00
10.00
12.00
10000 15000 20000 25000 30000
λ( )ae
[ ]Temperature K
1atm
10atm
=7n=12n
[ W m
-1 K
-1]
100atm
0.80
0.85
0.90
0.95
1.00
10000 15000 20000 25000 30000
λ( )a / λ( )u
[ ]Temperature K
1atm
10atm
100atm
=7n
=12n
e
e
In this case the presence of excited states affects only the interactions of electrons with H(n).
The figure reports the ratio λea/ λe
u calculated with the two sets of collision integrals as a function of temperature at different pressures.
Again we observe that the excited states increase their influence with increasing the pressure.
At high pressure the deviation decreases when considering only 7 excited states.
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Results IV: Reactive Thermal Conductivity
0.00
2.00
4.00
6.00
10000 15000 20000 25000
Temperature [K]
λ( )ar
1atm10atm
=7n
=12n
[ W m
-1 K
-1]
100atm
0.40
0.50
0.60
0.70
0.80
0.90
1.00
10000 15000 20000 25000
Temperature [K]
λ( )a / λ( )u
1atm
10atm
100atm
=7n
=12n
r
r
This contribution has been extensively analyzed in a previous paper*.
The main conclusions follow the trend illustrated for λh and λe in this work.
*M.Capitelli, P.Celiberto, C.Gorse, A.Laricchiuta, P.Minelli, D.Pagano, Phys. Rev. E 66,016403/1 (2002)
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Results V: Viscosity
0.0 100
5.0 10-5
1.0 10-4
1.5 10-4
10000 15000 20000 25000 30000
Temperature [K]
η( )a
1atm
10atm
=7n
=12n[ Kg m
-1 s
-1]
100atm
0.20
0.40
0.60
0.80
1.00
10000 15000 20000 25000 30000
Temperature [K]
η( )a / η( )u
1atm
10atm
100atm
=7n
=12n
The results for viscosity are in line with those discussed for the heavy particles translational contribution to the total thermal conductivity.
The viscosity values calculated with the “abnormal” cross sections (η(a)) are less than the corresponding results calculated with the “usual” cross sections (η(u)). The relative error decreases when, at high pressure, seven excited states are included in the calculation.
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Results VI: Electrical Conductivity
0.0 100
1.0 104
2.0 104
3.0 104
10000 15000 20000 25000 30000
σ( )ae
[ ]Temperature K
=7n
1atm
10atm
[ S m
-1]
100atm =12n
100atm
0.65
0.70
0.75
0.80
0.85
0.90
0.95
1.00
10000 15000 20000 25000 30000
σ( ) a/ σ
( )u
[ ]Temperature K
100atm
=7n
=12n
1atm
10atm
e
e
The trend of the electrical conductivity follows that one described for the contribution of electrons to the total thermal conductivity.
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Results VII: Number of levels in partition function
0.40
0.50
0.60
0.70
0.80
0.90
1.00
10000 15000 20000 25000 30000
λ( )a / λ( )u
[ ]Temperature K
h
h
=1n=2n
=4n
=6n( )a
0.80
0.85
0.90
0.95
1.00
10000 15000 20000 25000 30000
n=1
n=2
n=4
n=6
λ( )a / λ( )u
[ ]Temperature K
e
e
( )b
0.40
0.50
0.60
0.70
0.80
0.90
1.00
10000 15000 20000 25000 30000
n=1
n=2
n=4
n=6
Temperature [K]
λ( )a / λ( )u
r
r
( )c
Figures show the ratio between transport coefficients calculated by using “abnormal” and “usual” collision integrals at pressure of 1000 atm, as a function of temperature and for different number of atomic levels.
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0.40
0.50
0.60
0.70
0.80
0.90
1.00
10000 15000 20000 25000 30000
Temperature [K]
η( )a / η( )u
=1n=2n
=4n
=6n
( )e
0.75
0.80
0.85
0.90
0.95
1.00
10000 15000 20000 25000 30000
σ( ) a/ σ
( )u
[ ]Temperature K
e
e
=1n=2n
=4n
=6n( )f
At high pressure the number of excited states decrease. However increasing pressure, the ionization equilibrium is shifted to higher temperatures so that the concentration of low lying excited states can be sufficient to affect the transport properties
We can see that in this case already the first excited state (n=2) affects the results.
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Conclusions
The results reported indicate a strong dependence of the transport properties of LTE H2 plasmas on the presence of electronically excited states. This conclusion is reached when comparing the transport coefficients calculated with the two sets of collisison integrals.
Our results emphasize the importance of these states in affecting the transport coefficients specially at high pressure.
But at high pressure a question is open concerning the number of excited states to be included in the calculation of the partition function.
Another point to be discussed is the accuracy of the present calculations with respect to the Chapman-Enskog approximation used in the present work.
These approximations are very accurate when neglecting the presence of excited states. In the presence of excited states with their “abnormal” transport cross sections these approximations could not be sufficient.
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1. Excitation and de-excitation by electron impact
2. Ionization by electron impact and three body recombination
3. Spontaneous emission and absorption
4. Radiative recombination
Collisional-Radiative Model for Atomic Plasma
€
A(i)+e−(ε)kij⏐ → ⏐
k ji← ⏐ ⏐
A( j)+e−( ′ ε )
€
A(i)+e−(ε)kic⏐ → ⏐
kci← ⏐ ⏐
A+ +e−( ′ ε )+eb−(εb)
€
A(i) λijAij⏐ → ⏐ ⏐ A( j)+h ij with i> j
€
A+ +e−(ε) βi⏐ → ⏐ A(i)+h
![Page 29: Internal partition function calculated with where N is the particle density (cm 3 ) Influence of Electronically Excited States on Thermodynamic Properties.](https://reader030.fdocuments.net/reader030/viewer/2022032806/56649efe5503460f94c130c5/html5/thumbnails/29.jpg)
Rate Equations
€
dni
dt=+ njA ji
*
j>i∑ +ne njk ji
j≠i∑ +ne
2n+kci+nen+βi −ni A ij*
j<i∑ −nine kij
j≠i∑ −ninekic ∀i
€
dne
dt=dn+
dt=− dni
dti∑
Quasi-Stationary Solution(QSS)
€
dni
dt=0 ∀i
€
dni
dt≠0 ∀i
Stationary solution
Time-dependent solution
€
dni
dt=0 i≥2
dn1dt
≈−dne
dt=−dn+
dt
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QSS approximation
€
dni
dt=0 i≥2
dn1dt
≈−dne
dt=−dn+
dt
⎧
⎨ ⎪
⎩ ⎪
€
X i =ni
niSB
€
dX1dt
=a11X1+ a1jX jj=2
i*
∑ −b1
€
X i≥2 =X i≥20 +Ri≥2
1 X1
€
aijX jj=1
i*
∑ =bi i >1
The ground state density changes like the density of the charged particles andthe excited states are in an instantaneous ionization-recombination equilibrium with the free electrons
differential equation for the ground state
system of linear equation for excited levels
The system of equations is linear in X1
€
X i≥20 =f(ne,Te)
€
Ri≥21 =f(ne,Te)
Xj (j>1) can be calculated when X1, ne, Te are given
€
X i≥2 =f(X1,ne,Te)
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CR for Atomic Nitrogen Plasma: Energy-level Model
group Energy (cm-1) Statistical weight Terms1 0 4 2p34S2 19228 10 2p32D3 28840 6 2p32P4 83337 12 3s4P5 86193 6 3s”P6 95276 36 3p4S, 4P, 4D7 96793 18 3p2S,2P,2D8 103862 18 4s4P,2P9 104857 60 3d4P,4D,4F
10 104902 30 3d2P,2D,2F11 107125 54 4p4S,4P,4D,2S,2D,2P12 109951 18 5s4P,2P13 110315 90 4d4P,4D,4F,2P,2D,2F14 110486 126 4f4D,4F,4G,2D,2F,2G15 111363 54 5p4S,4P,4D,2S,2P,2D16 112691 18 6s4P,2P17 112851 90 5d4P,4D,4F,2P,2D,2F18 112955 288 5f,5g19 113391 54 6p20 114211 90 6d4P,4D,4F,2P,2D,2F21 114255 486 6f,6g,6h22 114914 882 n=723 115464 1152 n=824 115837 1458 n=925 116102 1800 n=1026 116298 2178 n=1127 116445 2592 n=1228 116560 3042 n=1329 116650 3528 n=1430 116724 4050 n=1531 116784 4608 n=1632 116834 5202 n=1733 116875 5832 n=1834 116910 6498 n=1935 116940 7200 n=20
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CR for Atomic Nitrogen Plasma with QSS
Xi vs level energy
Te=5800 K Te=11600 K Te=17400 K
0.0001
0.001
0.01
0.1
1
10
8 104 8.5 104 9 104 9.5 104 1 105 1.05 105 1.1 105 1.15 105 1.2 105
ne=10
8 cm
-3
ne=1016 cm-3
level energy (cm-1
)
X1=1
0.0001
0.001
0.01
0.1
1
10
8 104 8.5 104 9 104 9.5 104 1 105 1.05 105 1.1 105 1.15 105 1.2 105
ne=108 cm-3
ne=1016 cm-3
level energy (cm-1
)
X1=1
0.0001
0.001
0.01
0.1
1
10
100
8 104 8.5 104 9 104 9.5 104 1 105 1.05 105 1.1 105 1.15 105 1.2 105
ne=108 cm-3
ne=1016 cm-3
level energy (cm-1
)
X1=1
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Time-dependent solution
CR rate equations Boltzmann equation
€
dni
dt≠0 ∀i
Rate coefficients for electron impact processes
€
k= f(ε)Et
∞∫ σ(ε)v(ε)dεf(ε) electron energy distribution functionσ(ε) cross sectionv(ε) electron velocity
level populationplasma composition
f(ε)rate coefficients
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Atomic Hydrogen Plasma
P=100 Torr, Tg=30000 K, Te(t=0)=1000 K H+ = e
- =10-8 , H=1, H(1)=1, H(i)=0 i>1
€
H(n≤25),H+ ,e−[ ]
0
5000
10000
15000
20000
25000
30000
35000
10-14 10-12 10-10 10-8 10-6 10-4 10-2 100 102 104 106
time (s)
108
1010
1012
1014
1016
10-5 10-4 10-3 10-2 10-1
H
H+
e-
time (s)
10-20
10-18
10-16
10-14
10-12
10-10
10-8
10-6
0.0001
0.01
1
100
104
10-9 10-8 10-7 10-6 10-5 10-4 10-3 10-2 10-1
i=1i=2i=5i=10i=15i=20i=25
time (s)
density (cm-3) vs time(s) Xi = ni/niSB vs time(s) Te vs time(s)
![Page 35: Internal partition function calculated with where N is the particle density (cm 3 ) Influence of Electronically Excited States on Thermodynamic Properties.](https://reader030.fdocuments.net/reader030/viewer/2022032806/56649efe5503460f94c130c5/html5/thumbnails/35.jpg)
10-30
10-28
10-26
10-24
10-22
10-20
10-18
10-16
10-14
10-12
10-10
10-8
10-6
0.0001
0.01
1
0 5 10 15 20 25
t(s)=0 s
t(s)=10-10 s
t(s)=10-9 s
t(s)=5 10-9 s
t(s)=10-8 s
t(s)=3 10-8 s
t(s)=5 10-8 s
t(s)=8 10-8 s
t(s)=10-7 s
t(s)=10-6 s
t(s)=10-5
s
t(s)=10-4 s
t(s)=8 10-4 s
t(s)=9 10-4 s
t(s)=10-3 s
ε( )eV
Tfit = 30020 K
H(i)/g(i) vs Ei
10-30
10-28
10-26
10-24
10-22
10-20
10-18
10-16
10-14
10-12
10-10
10-8
10-6
0.0001
0.01
0 2 4 6 8 10 12 14
t(s)=0 s
t(s)=10-10
s
t(s)=10-9
s
t(s)=5 10-9 s
t(s)=10-8 s
t(s)=3 10-8 s
t(s)=5 10-8 s
t(s)=8 10-8 s
t(s)=10-7 s
t(s)=10-6 s
t(s)=10-5 s
t(s)=10-4 s
t(s)=8 10-4 s
t(s)=9 10-4 s
t(s)=10-3 s
( )level energy eV
Tfit = 29986 K
eedf(eV-3/2) vs E
![Page 36: Internal partition function calculated with where N is the particle density (cm 3 ) Influence of Electronically Excited States on Thermodynamic Properties.](https://reader030.fdocuments.net/reader030/viewer/2022032806/56649efe5503460f94c130c5/html5/thumbnails/36.jpg)
rese
rvoi
rexit
throat
Non-Equilibrium Kinetics in High EnthalpyNozzle Flows
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coupling state-to-state kinetics with fluid dynamic models
- Numerical aspects- Coupling with kinetics
- Numerical aspects- Coupling with kinetics
- Chemical kinetics- Vibrational kinetics- Metastable state kinetics
- Chemical kinetics- Vibrational kinetics- Metastable state kinetics
- Boltzmann equation- Coupling with chemical kinetics- EM fields contribution
- Boltzmann equation- Coupling with chemical kinetics- EM fields contribution