#Problem constants:
domainLength=5.0e-03		#in meters
constantPressure=1		#1=isobaric, 0=isochoric
dPdt=0.0e0			#Units: Pa/s
problemType=0			#0=heatsource to ignite(premix),1=premix, 2=custom initial condition
reflectProblem=0		#If 1, the initial conditions are reflected across the center of the domain. Useful for spherically imploding flames for instance.
mdot=0.0
initialTemperature=300.0	#in Kelvin
initialPressure=1.0		#in atmospheres
gasFile=nitrogenPlasma.cti	#File containing thermodynamic, kinetic, and transport info
gasPhase=gas
transportPhase=transport
transportModel=Mix		#Transport model
mixtureComposition=N2:1.0	#Mole Fractions!
crossFile=N2.dat
metric=1			#0=planar,1=cylindrical,2=spherical
heatType=1
ignTime=9e-04			#Time over which energy is supplied in seconds
QDot=6.8e10			#Power supplied in units of W/m3
heatFile=discharge.csv
radFile=rad.csv
therCondFile=therCondAirPlasma.csv
kernelSize=0.5e-03
mixingWidth=0.6e-03		#mixing layer width in m (for diffusion problem)
shift=4e-03		#shift of mixing layer into domain (for diffusion problem)
dirichletInner=0		#Boundary conditions for scalars (T,Y)
dirichletOuter=0
wallTemperature=300.0
#Grid settings:
adaptiveGrid=0
moveGrid=0
Rg=300
gridOffset=0
basePts=1000
gridDensitySlope=70.0e0
fineGridHalfWidth=8e-03
gridRefinement=1000.0e0;
leftRefineFactor=0.01
rightRefineFactor=0.01
refineLeft=1
refineRight=1
position=0.0
isotherm=1000.0
#Solver settings:
nSaves=100			#Save solution every nSaves timesteps
writeEveryRegrid=0
writeRates=0
relativeTolerance=1e-06
radiusTolerance=1e-09		#absolute tolerance for radius
temperatureTolerance=1e-09
pressureTolerance=1e-09
massFractionTolerance=1e-09
bathGasTolerance=1e-09
electronTolerance=1e-15
finalTime=1.0e0			#in seconds
setConstraints=0
suppressAlg=0
nThreads=1
printYdot=0
printY=0
dryRun=0
