plasma assisted combustion...afosr muri november 9 –10, 2011 fundamental mechanisms, predictive...
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Plasma Assisted Combustion:Discharge Energy Balance, Bootstrap Effect in Plasma-Chemical Kinetics
1. Nano-Second Pulse Plasma Ignition Below Self-Ignition Threshold• LIF, PLIF, CRD Experiments
2. Energy Efficiency of Plasma Assisted Combustion• Kinetic Modeling of Discharge Energy Balance • Combustion Assisted Plasma • Modeling of Bootstrap Effect in PAC
AFOSR MURI ● November 9-10, 2011Fundamental Mechanisms, Predictive Modeling, and Novel Aerospace Applications of Plasma Assisted Combustion
Modified Team:
AlexanderFridman
MikhailPekker
LiangWu
DanilDobrynin
AndreyStarikovskiy
NickCernansky
DavidMiller
Energy Efficiency of Plasma Assisted Combustion (Scramjet)Kinetic Modeling of Active Species Energy Cost in Different Discharges
AFOSR MURI ● November 9 – 10, 2011Fundamental Mechanisms, Predictive Modeling, and Novel Aerospace Applications of Plasma Assisted Combustion
7.4 ns
Streamer Discharge (300 Td)
Dielectric Barrier Discharge
PAC Energy Efficiency, Modeling of Transitional DischargesCombustion Assisted Plasma, 1D Methane-Air Modeling
o If W ≈ 10 eV, G~10 (transitional discharges, microwave/gliding arcs, non-premixed: collective effects)
• 0.01 eV/mol (≈ 30 K)• specific enthalpy H ≈ 0.03
MJ/kg • total flow enthalpy 1.5 – 2.5
MJ/kg at M = 5 – 7• power 10 MW/m2
o If W ≈ 0.3 – 1 eV, G~100-300 (transitional discharges, partially premixed, combustion assisted plasma; Gmax, exp ~ 3000 for PO)
• 0.0003 - 0.001 eV/mol (1-3 K)• specific enthalpy H ≈ 1 – 10
kJ/kg • total flow enthalpy 1.5 – 2.5
MJ/kg at M = 5 – 7• power 0.3 – 1 MW/m2
AFOSR MURI ● November 9 – 10, 2011Fundamental Mechanisms, Predictive Modeling, and Novel Aerospace Applications of Plasma Assisted Combustion
Gliding Arc
GAT
MW
Not only radicals/excited species/ions but easy-to-ignite intermediates (CH2O, CH3OH, etc.) play role in PAI
Nano-Second Pulse Plasma Ignition Below Self-Ignition Threshold
Laser Induced Fluorescence
Methane 300 K
OH Planar LIF
Cavity Ring-Down Spectroscopy
• Three different diagnostic methods
• Homogeneous [OH] distribution along
the discharge channel
• Long life time of OH at low
temperature below ignition threshold
Methane 500 K @2 μs delay
AFOSR MURI ● November 9 – 10, 2011Fundamental Mechanisms, Predictive Modeling, and Novel Aerospace Applications of Plasma Assisted Combustion
Time resolved PLIF and CRDS diagnostics of OH radicals in the afterglow of plasma discharge in hydrocarbon mixtures
•Methane / Air mixture•Equivalence ratio: Lean (φ=0.1)•Temperature regimes:
Room temperature, 300 KElevated temperature, 500 K
•Premixed and preheated flowFlow rate ~20 cm/s
Liang Wu, J. Lane, N. Cernansky, D. Miller, A. Fridman, A. Starikovskiy, 7th US National Combustion Meeting, Atlanta, March 20-23, 2011
PLIF diagnostics has shown quite homogeneous
distribution of OH formation along the discharge channel
CRDS has provided the absolute [OH] which can be further
used for kinetic model development
Liang Wu, J. Lane, N. Cernansky, D. Miller, A. Fridman, A. Starikovskiy, 7th US National Combustion Meeting, Atlanta, March 20-23, 2011
Time resolved PLIF and CRDS diagnostics of OH radicals in the afterglow of plasma discharge in hydrocarbon mixtures
What causes the oxidation chemistry in afterglow?
T = 300 K 1D CH4-Air Mixture Kinetic Modeling (Konnov & GRI Mechs) with Analysis of Contribution of:1. Plasma generated radicals (O, OH ~10-4 – 10-3)
• Disappear within ~1-10 ms
2. Positive and negative ion catalysis (lifetime ~10 ms, low contribution, Langevin model)• HO2 + H2(M+) → OH + H2O + M+
• O2- + H2 → OH- +OH
• OH- + H(HO2) → H2O (+O2) + e• e + O2(+M) → O2
-
3. Plasma generated NO (~10-3 – 10-2, low contribution)• NO + HO2 → NO2 + OH• H + NO2 → NO + OH
4. Plasma generated excited species (unknown kinetics, alpha model)• HO2(group) + (N2
*) → OH + O + N2
• CH3O2 + (N2*) → CH2O + OH + N2
5. “Bootstrap” effect• Indirect effect of plasma (change of
macroparameters: T, stable components)• Plasma chemistry/reforming add’l heating• Plasma chemistry/reforming change of mixture
T = 500 K
Plasma assisted combustion mechanisms
Plasma catalysis
Chain reactions sustained by ions and excited species
Bootstrap effect
• Indirect effect of plasma (change of macroparameters:
temperature and stable components) to shorten ignition delay
• Plasma chemistry/reforming additional heating due
to chain oxidation by primary plasma species
• Plasma chemistry/reforming change of mixture due
to chain oxidation by primary plasma species (formation of
small amount of easy-to-ignite stable species)
Munchausen effect
Thermal effectNon-Thermal Radical effect
Radical chains terminate below autoignition limit
Bootstrap Effect in Plasma-Assisted Ignition (Atmospheric Pressure Methane-Air Mixture at Temperatures Below Auto-Ignition Limit)
Heating due to radicals: 12K
Kinetic Modeling (Konnov’s Mechanism); T0 = 960 K, direct discharge heating: 40 K, 10-3 [O]
Disappearance of radicals
Accumulation of easy-to-ignite stable species
Ignition delay
Bootstrap effect: plasma induced change of primary ignition macroparameters (T, Comp.)
OH OCHOCH
OH CHCHOH
22 3
2 34
Bootstrap coefficient:
Effective increase of temperature
exceeds direct plasma heating
heat
compRheat
heat
0eff
compRheat0eff
ΔT
ΔTΔTΔT
ΔT
TTK
ΔTΔTΔTTT
For the example above: K=3
DTheat – Direct heat 40KDTR – Heat due to radicals 12KDTcomp – Effective heating due to
change of composition (CH2O) 68K
Bootstrap Effect in Methane-Air Mixture:change of composition (plasma reforming, CH2O) contributes more than radical heating
Direct heating:[CH4]=0.0944, [O2]= 0.189 [N2]=0.7130 [O]=0.001T0=960K, P0=1atm. G-factor for O = 6.0===========================DTheat =40K
[O]=0.001Tin=DTheat+T0=40+960=1000[K]
Temperaturebefore discharge
Direct Heating
Bootstrap effect
Heatingdue to
Radicals
Effective Heatingdue
to change of composition
960K DTheat=40 K
DTR=12 K DTcomp=68K
3ΔT
ΔTΔTΔTK
heat
compRheat
Bootstrap Effect in Methane-Air Mixture:effect of initial temperature, 5·10-4 [O]
Bootstrap Effect in Methane-Oxygen Mixture
Direct heating (estimation):[CH4]= 0.0944, [O2] = 0.9051 [O] = 0.0005T0=979K, P0=1atm.G-factor for O = 8.0
DTheat=15.6K [O]=0.0005T0=DTheat+Tin=15.6+984.6=1000[K]
Temperaturebefore discharge
Direct Heating
Bootstrap effect
Heatingdue to
Radicals
Effective Heating due to change of composition
984.6K DTheat=15.6 K
DTR=21 K DTcomp=83.3 K
D
OH OCHOCH
OH OCHOCH
OH CHCHOH
2
1
2 3
22 3
2 34
[O2(1D)]=0.002
OH OCHOCH
OH CHCHOH
22 3
2 34
Bootstrap Effect in Ethylene-Air Mixturequazi-stable intermediates CH2O, HO2
22
342
HOCOOHCO
OHCOOHCO
HCOCHOHC
3242
223
CHOCHOHHC
OHOCHOCH
Production of radicals and HO2
Chain reactions
0
0.0002
0.0004
0.0006
0.0008
0.001
0 0.00001 0.00002 0.00003 0.00004 0.00005
Time(s)
O
OH
HO2
CO
CH3
CH2O
850
852
854
856
858
860
862
864
0 0.00001 0.00002 0.00003 0.00004 0.00005
T[K
]
Time(s)
Direct heating (estimation):[C2H4]= 0.066, [O2] = 0.198 [N2]=0.735[O] = 0.001 P0=70tor.
DTheat=42.4 K [O]=0.001T0=DTheat+Tin=42.4+807.6=850 [K]
Bootstrap Effect in Ethylene-Air Mixture
0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 5 5.5 6 6.5 7
1000
1200
1400
1600
1800
2000
2200
2400
2600
Time(s)
T
[K]
T=850 O=0.0001
T=850
T=865
T=865 CH2+Radicals
T=865 H2O
K=3.2Teffect=943K
Temperaturebefore discharge
Direct Heating
Bootstrap effect
Heatingdue to
Radicals
Effective Heating due to change of composition
807.6 K DTheat=42. 4K
DTR=15. 4K DTcomp=77.6K
T[K] [O] [CH3]+[OH] [CH2O] [HO2] Delay time (s)
850 0 0 0 0 6.75
850 0.001 0 0 0 0.675
865 0 0 0 0 4.61
865 0 0.0003+0.000016 0.000537 0 1.052
865 0 0 0 0.000232 0.756
Direct heating (estimation):[C2H4]= 0.066, [O2] = 0.198 [N2]=0.735[O] = 0.001 P0=70tor.
DTheat=42.4 K [O]=0.001T0=DTheat+Tin=42.4+807.6=850 [K]
quazi-stable intermediates CH2O, HO2
Plasma assisted combustion mechanisms
Plasma catalysis
Chain reactions sustained by ions and excited species
Bootstrap effect
• Indirect effect of plasma (change of macroparameters:
temperature and stable components) to shorten ignition delay
• Plasma chemistry/reforming additional heating due
to chain oxidation by primary plasma species
• Plasma chemistry/reforming change of mixture due
to chain oxidation by primary plasma species (formation of
small amount of easy-to-ignite stable species)
Munchausen effect
Thermal effectNon-Thermal Radical effect
Radical chains terminate below autoignition limit
Plasma Fuel Reforming vs Plasma Assisted Ignition
CH4
[L/min]
Air
[L/min]
[O/C] W
[watt]
From Discharge
[eV/molec]
From Reaction
[eV/molec]
Total
[eV/molec]
Add Air
[L/min]
Total
[eV/Molec]
5.39 20.09 1.55 480 0.26 0.074 0.34 (DT≈876K) 31.42 0.15 (DT≈390K)
Ignition temperature
about 700K
H2 CO CO2 N2 CH4 C2H4 C2H2 O2
12.15 5.97 0.50 60.74 12.043 0.21 0.79 9.59
Reforming Mixture
CH4 + Air Reforming Mixture +Air
T=1025K(delay ⋍ 0.1s) T= 850 K(delay 0.1s)
AFOSR MURI ● November 9 – 10, 2011Fundamental Mechanisms, Predictive Modeling, and Novel Aerospace Applications of Plasma Assisted Combustion
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