Table 10.3: Alphabetical Listing of Keywords [P-S]
Keyword |
Definition | |||
---|---|---|---|---|
Reactor Property |
Pressure before the incident shock. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Pressure |
Required |
atm |
P1A 1.0 | |
Keyword Usage |
Optional Keyword. The shock velocity and any two of temperature, pressure, or density must be specified for conditions before the incident shock. See also T1 and RHO1 . | |||
Reactor Models |
| |||
Reactor Property |
Pressure after the incident shock. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Pressure |
Required |
atm |
P2A 2.3 | |
Keyword Usage |
Optional Keyword. Any two of temperature, pressure, or density must be specified for conditions after the incident shock. See also T2 and RHO2 . | |||
Reactor Models |
| |||
Reactor Property |
Pressure after the reflected shock, given as in the equations. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Pressure |
Required |
atm |
P3A 2.3 | |
Keyword Usage |
Optional Keyword. Any two of temperature, pressure, or density must be specified for conditions before the reflected shock. See also T3 and RHO3 . | |||
Reactor Models |
| |||
Output |
Partial-pressures of the gas-phase species will be used in the diagnostic output file. | |||
Keyword Usage |
Optional keyword. By default, mass fractions are printed, not partial pressures. | |||
Reactor Models |
| |||
Output |
This keyword resets all bulk species densities defined in the surface mechanism to the value given by this keyword. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
material_name |
Required |
None | PBDEN ligA 2.15 | |
bulk_density |
Required | g/cm3 | PBDEN ligA 2.15 | |
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Output |
Request the probability distribution of a scalar to be output to a pdf.plt file. Any number of PDF entries is allowed. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Scalar (temperature or species name) |
Required |
-- |
PDF T | |
Keyword Usage |
Optional keyword. By default, no PDF is printed. | |||
Reactor Models |
| |||
Reactor Property |
Include the energy conservation equation for particles. | |||
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Reactor Property |
Specifies an estimate of the equilibrium pressure. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Pressure |
Required |
atm |
PEST 1.1 | |
Keyword Usage |
Optional keyword. May help convergence to the equilibrium pressure, or assure an appropriate equilibrium pressure is calculated when a second, trivial solution exists. | |||
Reactor Models |
| |||
Output |
Analyze the pressure fall-off of a gas phase reaction, that is, creates a table of reaction rates versus total gas pressure at a constant temperature. The ALL option is the default and produces tables for every gas-phase reaction. The NONE option suppresses output for all of the reactions. If reaction information is desired for only certain reactions, they may be optionally specified by their number (given in the Pre-processor output) or by typing an exact duplicate of the reaction expression (see example input). | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
ALL option |
Optional, default is ALL |
-- |
PFAL ALL | |
NONE option |
Optional, default is ALL |
-- |
PFAL NONE | |
Gas reaction number list |
Optional, default is ALL |
-- |
PFAL 2 5 | |
Gas reaction expression |
Optional, default is ALL |
-- |
PFAL 2CH3(+M)<=>C2H6(+M) | |
Keyword Usage |
Optional keyword. By default, the table output is determined by the ALL or NONE keyword. | |||
Reactor Models |
| |||
Reactor Property |
Set the minimum bounds of the particle moments to a slightly negative number to allow the solver more room to search for a solution. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Minimum bound |
Required |
-- |
PFLR -1.0d-06 | |
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Problem Type |
Constant pressure and enthalpy constraints. | |||
Keyword Usage |
Optional keyword. Exactly one problem type keyword must be included. | |||
Reactor Models |
| |||
Notes |
HP keyword is equivalent. | |||
Reactor Property | Specified mass outflow rate of the phase. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
phase name |
Required |
|
PHASE_MASSOUTFLOWRATE urea 0.0 | |
mass outflow rate of the phase |
Required |
g/sec |
PHASE_MASSOUTFLOWRATE urea 0.0 | |
Keyword Usage |
Optional keyword. Bulk name must follow the keyword. "Gas" is not valid for the keyword. | |||
Reactor Models |
| |||
Reactor Property | Specified molar outflow rate of the phase. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
phase name |
Required |
|
PHASE_MOLAROUTFLOWRATE urea 0.0 | |
molar outflow rate of the phase |
Required |
mole/sec |
PHASE_MOLAROUTFLOWRATE urea 0.0 | |
Keyword Usage |
Optional keyword. Bulk name must follow the keyword. "Gas" is not valid for the keyword. | |||
Reactor Models |
| |||
Reactor Property | Specified volumetric outflow rate of the phase. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
phase name |
Required |
|
PHASE_VOLOUTFLOWRATE urea 0.0 | |
volumetric outflow rate of the phase |
Required |
cm3/sec |
PHASE_VOLOUTFLOWRATE urea 0.0 | |
Keyword Usage |
Optional keyword. Bulk name must follow the keyword. "Gas" is not valid for the keyword. | |||
Reactor Models |
| |||
Reactor Property | Specified volume of the phase. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
phase name |
Required |
|
PHASE_VOLUME urea 10.0 | |
volume of the phase |
Required |
cm3 |
PHASE_VOLUME urea 10.0 | |
Keyword Usage |
Optional keyword. Bulk name must follow the keyword. "Gas" is not valid for the keyword. | |||
Reactor Models |
| |||
Reactor Property |
Set the upper limit of the pressure range (in atmospheres) in tables where the gas pressure is varied. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Pressure |
Required |
atm |
PHIA 2. | |
Keyword Usage |
Optional keyword. By default, the pressure is 1.315789 atm (1000 Torr). | |||
Reactor Models |
| |||
Notes |
| |||
Reactor Property |
Use a planar coordinate system, which is appropriate for a Tsuji burner configuration. | |||
Keyword Usage |
Optional keyword. By default, the coordinate system is radial and axisymmetric. | |||
Reactor Models |
| |||
Reactor Property |
Use a plateau profile to set up initial solution estimates, rather than a linear profile. | |||
Keyword Usage |
Optional keyword. By default, the plateau profile is used. | |||
Reactor Models |
| |||
Reactor Property |
Set the lower limit of the pressure range (in atmospheres) in tables where the gas pressure is varied. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Pressure |
Required |
atm |
PLOA 1.0 | |
Keyword Usage |
Optional keyword. By default, the pressure is 0.001315789 atm (1 Torr) | |||
Reactor Models |
| |||
Notes |
| |||
Reactor Property |
Indicates that plug-flow equations will be solved and that the Reactor Model will be one of the family of Plug Flow Reactors. | |||
Keyword Usage |
Required keyword. | |||
Reactor Models |
| |||
Reactor Property |
Assigns the initial (or estimate for steady-state calculations) number density of the particle consisting of the designated bulk species. The default value is 0. The reactor number is optional. When no reactor number is given, the same initial number density will apply to all reactors in the network. If neither PVFE nor PROE is given, the initial/estimate values of the moments are computed as
| |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material name |
Required |
-- |
PNDE CARBON 1.0E10 4 | |
Number density |
Required |
particles/cm3 |
PNDE CARBON 1.0E10 4 | |
Reactor number |
Optional |
-- |
PNDE CARBON 1.0E10 4 | |
Keyword Usage |
Optional keyword. The default value is value for the number density is 0. | |||
Reactor Models |
| |||
Inlet Property |
Assigns the number density of the particle consisting of the designated material name to the named inlet stream. The default value is 0. The stream name is optional if there is only one inlet. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Stream name |
Optional if only one inlet. |
-- |
PNDI exhaust CARBON 1.0E12 | |
Material name |
Required |
-- |
PNDI exhaust CARBON 1.0E12 | |
Mass density |
Required |
particles/cm3 |
PNDI exhaust CARBON 1.0E12 | |
Keyword Usage |
Optional keyword. The default value for the mass density is 0. | |||
Reactor Models |
| |||
Reactor Property |
Set the total number of pressure entries in tables where the gas pressure is varied. The default is 10. Note that the changes in the pressure are determined on a logarithmic scale. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Number of pressures |
Required |
-- |
PNUM 10 | |
Keyword Usage |
Optional keyword. By default, the number of pressures is 10. | |||
Reactor Models |
| |||
Reactor Property |
Specify intake-side piston pin offset distance (optional). | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Offset distance |
Required |
cm |
POLN1 0.5 | |
Keyword Usage |
Optional keyword. Optional for use with OPMV or OPOC. Default value = 0.0. | |||
Reactor Models |
| |||
Reactor Property |
Specify exhaust-side piston pin offset distance (optional). | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Offset distance |
Required |
cm |
POLN2 1.1 | |
Keyword Usage |
Optional keyword. Optional for use with OPMV or OPOC. Default value = 0.0. | |||
Reactor Models |
| |||
Reactor Property Profiles |
Reactor pressure profile specified as a function of time for transient 0-D homogeneous systems or as a function of distance for Plug Flow Reactors. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Time or Distance value, depending on Reactor Model |
Required |
sec or cm |
PPRO 1.0E-4 1.0 | |
Pressure |
Required |
atm |
PPRO 1.0E-4 1.0 | |
Reactor number (PSR clusters only) |
Optional If no number is given, the profile described by the first two values is assumed to apply to all reactors in a cluster. |
-- |
PPRO 1.0E-4 1.0 1 | |
Keyword Usage |
Optional keyword. By default, no profile is provided. | |||
Reactor Models |
| |||
Reactor Property |
The Prandlt number used in the generalized heat transfer correlation. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Prandlt number |
Required |
-- |
PRDL 0.77 | |
Keyword Usage |
Optional keyword. By default, the value is 0.7. | |||
Reactor Models |
| |||
Reactor Property |
The reactor pressure in atmospheres. Depending on the Reactor Model and problem type, the pressure specified can serve as the pressure constraint (for constant-pressure problems), as an initial guess for pressure (for steady-state problems where pressure is a variable), or as the initial reactor pressure (for transient cases where pressure is a variable). For the Mechanism Analyzer, this is the bath-gas pressure. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Reactor pressure |
Required |
atm |
PRES 1.0 | |
Reactor number (PSR clusters only) |
Optional If no number is given, the keyword is assumed to apply to all reactors in a cluster. |
-- |
PRES 1.0 1 | |
Keyword Usage |
Required keyword in most cases. Optional keyword only for Mechanism Analyzer, where the default is 1 atm. | |||
Reactor Models |
| |||
Notes |
| |||
Reactor Property |
Minimum mole fraction value applied to the estimated values of the flame products, when the (default) equilibrium is used to determine product estimates. Ignored in the case that PROD2 keywords are present. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Product fraction |
Required |
mole fractions |
PRMN 1.0E-10 | |
Keyword Usage |
Optional keyword. By default, the flame product fraction is set to 0. | |||
Reactor Models |
| |||
Output |
Printing control. "PRNT 0" provides printed output for only the solution (plus sensitivity coefficients and rates-of-production coefficients, when requested). "PRNT 1" provides an additional summary of the iteration path from the solver. "PRNT 2" includes printing at every stage of the Twopnt solver’s Newton iteration and time stepping procedure. More printing is sometimes helpful when diagnosing problems and trying to adjust the input parameters to optimize convergence. However, since the increased printing requires more function evaluations to show how the solution is progressing, the computer time increases with increased printing. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Print control number |
Required |
-- |
PRNT 1 | |
Keyword Usage |
Optional keyword. By default, the print control is set to 1. | |||
Reactor Models |
| |||
Reactor Property |
Estimated values of the gas-phase mole fractions at the far end of the domain (that is, the deposition surface for CVD reactors or the burned state at XEND for Premixed Laminar Flames) or in the middle of the flame (for Opposed-flow Flames). The sum of the product mole fractions should equal to 1.0; if they do not, then a warning message will be printed to the diagnostic output file and the mole fractions will be normalized so that they do sum to one. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Species name |
Required |
-- |
PROD H2O 0.5 | |
Mole fraction |
Required |
-- |
PROD H2O 0.5 | |
Keyword Usage |
Optional keyword. If PROD2 keywords are not provided, then an equilibrium calculation will be used to determine the estimated product composition (see also PRMN). | |||
Reactor Models |
| |||
Notes | ||||
Reactor Property |
Assigns the initial (or estimate for steady-state calculations) number density of the particle consisting of the designated material name. The default value is 0. The reactor number is optional. When no reactor number is given, the same initial particle mass density will apply to all reactors in the network. The PROE keyword must be used in conjunction with the PNDE keyword and is mutually exclusive to keyword PVFE. When both PNDE and PROE are given, the moments are calculated as where is the mass of a material name molecule and is the mass density of the bulk material. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material name |
Required |
-- |
PROE CARBON 1.0E-10 1 | |
Mass density |
Required |
gm/cm3 |
PROE CARBON 1.0E-10 1 | |
Reactor number |
Optional |
-- |
PROE CARBON 1.0E-10 1 | |
Keyword Usage |
Optional keyword. The default value for the mass density is 0. PNDE keyword required. Cannot be used with PVFE. | |||
Reactor Models |
| |||
Inlet Property |
Assigns the mass density of the particle consisting of the designated material name to the named inlet stream. The default value is 0. The stream name is optional if there is only one inlet. The PROI keyword must be used in conjunction with the PNDI keyword and is mutually exclusive to keyword PVFI. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Stream name |
Optional if there is only one inlet. |
-- |
PROI EGR CARBON 1.0E-10 | |
Material name |
Required |
-- |
PROI EGR CARBON 1.0E-10 | |
Number density |
Required |
gm/cm3 |
PROI EGR CARBON 1.0E-10 | |
Keyword Usage |
Optional keyword. Must be used with PNDI. Cannot be used with PVFI. The default value for the number density is 0. | |||
Reactor Models |
| |||
Problem Type |
Constant pressure and entropy constraints. | |||
Keyword Usage |
Optional keyword. Exactly one problem-type keyword must be included. | |||
Reactor Models |
| |||
Notes |
| |||
Reactor Property |
The piston head area to bore area ratio. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Ratio of piston head area to bore area. |
Required |
None | PSBAR 1.1 | |
Keyword Usage |
Optional keyword. Default = 1.0. | |||
Reactor Models |
| |||
Notes | PSBAR should be > 1.0. | |||
Inlet Property |
Initial surface coverage on particles by the surface site species in the inlet flow. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Stream name |
Optional if there is only one inlet. |
-- |
PSURF inlet1 C(S) 0.1 | |
Surface species name |
Required |
-- |
PSURF inlet1 C(S) 0.1 | |
Surface coverage |
Required |
-- |
PSURF inlet1 C(S) 0.1 | |
Keyword Usage |
Optional keyword | |||
Reactor Models |
| |||
Solver |
Pseudo-velocity for use in modifying the surface species equations for improved convergence. This pseudo-convection term is incorporated into the surface site fraction equations in order to convert algebraic equations to differential equations. The value of the PSV should be small enough such that it has no effect on the solution results, but large enough to affect the convergence behavior. If not supplied, then the unmodified equations are used. The modified equations are sometimes helpful in reaching steady-state conditions for problems with stiff surface chemistry (e.g. catalytic combustion), but should not be used if no convergence problems are encountered. A recommended value to try for PSV would be about 1/10th of the inlet velocity, but the simulation should be repeated with smaller or larger values to make sure that it has no effect on the solution. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Pseudo-velocity |
Required |
cm/sec |
PSV 10. | |
Keyword Usage |
Optional keyword. By default, the value is set to 10* ATOL. | |||
Reactor Models |
| |||
Reactor Property |
The number of sections to use for the specified material. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material name |
Required |
-- |
PTM_SECTION_NUM SOOT 30 | |
Number of sections |
Required |
-- |
PTM_SECTION_NUM SOOT 30 | |
Keyword Usage |
Required when the Sectional Model is used. | |||
Reactor Models |
| |||
Reactor Property |
Tanh function constant that is used to blend lower and upper bounds of collision efficiency. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material name |
Required |
None |
PTM_SECTION_SIZEDEP_A0 SOOT 5 | |
A0 |
Required |
None |
PTM_SECTION_SIZEDEP_A0 SOOT 5 | |
Keyword Usage |
Optional keyword. Default size is 7. | |||
Reactor Models |
| |||
Reactor Property |
Use size-dependent collision efficiency for particles . | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material name |
Required |
None |
PTM_SECTION_SIZEDEP_COLEFF SOOT | |
Keyword Usage |
Optional keyword. Not used by default. | |||
Reactor Models |
| |||
Reactor Property |
Limit diameter for size-dependent collision efficiency. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material name |
Required |
None |
PTM_SECTION_SIZEDEP_DSTAR SOOT 13-06 | |
Diameter |
Required |
None |
PTM_SECTION_SIZEDEP_DSTAR SOOT 13-06 | |
Keyword Usage |
Optional keyword. No default value is given and must be specified by user when using size-dependent collision efficiency. For soot simulation, the value generally ranges from 10 to 20 nm. | |||
Reactor Models |
| |||
Reactor Property |
Hamaker constant for computing potential well depth when using size-dependent collision efficiency for particles. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material name |
Required |
None |
PTM_SECTION_SIZEDEP_HAMAKER SOOT 5e-13 | |
Diameter |
Required |
None |
PTM_SECTION_SIZEDEP_HAMAKER SOOT 5e-13 | |
Keyword Usage |
Optional keyword. Default value is 7e-13 erg. | |||
Reactor Models |
| |||
Reactor Property |
Number of "atoms" in the smallest section for the specified material. When etching reactions are present, the number of sectional atoms parameter needs to be unity. When only growth is present, the user can give some higher value to avoid calculations for smaller particles that will never be present. However, this value must not be greater than the number of atoms in the smallest nucleating particle. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material name |
Required |
-- |
PTM_SECTION_SN0 SOOT 1 | |
Number of sectional "atoms" |
Required |
-- |
PTM_SECTION_SN0 SOOT 1 | |
Keyword Usage |
Required when the Sectional Model is used. | |||
Reactor Models |
| |||
Reactor Property |
Geometric spacing factor to be used for sections. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material name |
Required |
-- |
PTM_SECTION_SPACING CARBON 2.0 | |
Geometric spacing factor |
Required |
-- |
PTM_SECTION_SPACING CARBON 2.0 | |
Keyword Usage |
Required when the Sectional Model is used. | |||
Reactor Models |
| |||
Reactor Property |
Thermal conductivity of particle material. This is a required input when any of the flame models are using the Sectional Model with thermophoresis. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material name |
Required |
-- |
PTM_SECTION_TCOND CARBON 2.0E+05 | |
Thermal conductivity of "material" |
Required |
erg/s-cm-K |
PTM_SECTION_TCOND CARBON 2.0E+05 | |
Keyword Usage |
Required when the Sectional Model with thermophoresis is used. | |||
Reactor Models |
| |||
Reactor Property | User-specified enhancement factor for the growth/etching reactions on particles. This can be used only with the sectional method. Note that the user-routines library must be compiled and linked; see the Chemkin Application Programming Interface Manual for details. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material name |
Required |
None |
PTM_SECTION_USERBULKROP CARBON | |
Keyword Usage |
Optional keyword. Not used by default. | |||
Reactor Models |
| |||
Reactor Property |
Signals that sectional model is to be used. This is a required keyword when the Sectional Model is used. | |||
Keyword Usage |
Required when the Sectional Model is used. | |||
Reactor Models |
| |||
Problem Type |
Constant pressure and volume constraints. | |||
Keyword Usage |
Optional keyword. Exactly one problem-type keyword must be included. | |||
Reactor Models |
| |||
Notes |
| |||
Reactor Property |
Assigns the initial (or estimate for steady state calculations) number density of the particle consisting of the designated material name. The default value is 0. The reactor number is optional. When no reactor number is given, the same initial particle volume fraction will apply to all reactors in the network. The PVFE keyword must be used in conjunction with the PNDE keyword and is mutually exclusive to keyword PROE. When both PNDE and PVFE are given, the moments are calculated as where is the mass of a material name molecule and is the mass density of the bulk material. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material name |
Required |
-- |
PVFE CARBON 1.0E-10 4 | |
Volume fraction |
Required |
cm3/cm3 |
PVFE CARBON 1.0E-10 4 | |
Reactor number |
Optional |
-- |
PVFE CARBON 1.0E-10 4 | |
Keyword Usage |
Optional keyword. The default value is value for the volume fraction is 0. PNDE keyword required. | |||
Reactor Models |
| |||
Inlet Property |
Assigns the volume fraction of the particle consisting of the designated material name to the named inlet stream. The default value is 0. The stream name is optional if there is only one inlet. The PVFI keyword must be used in conjunction with the PNDI keyword and is mutually exclusive to keyword PROI. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Stream name |
Optional if there is only one inlet. |
-- |
PVFI inlet1 CARBON 1.0E--9 | |
Material name |
Required |
-- |
PVFI inlet1 CARBON 1.0E-9 | |
Number density |
Required |
cm3 /cm3 |
PVFI inlet1 CARBON 1.0E-9 | |
Keyword Usage |
Optional keyword. Must be used with PNDI. Cannot be used with PROI. The default value for the number density is 0. | |||
Reactor Models |
| |||
Reactor Property |
Specify the reference gas viscosity at the reference temperature of the power-law for viscosity. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Reference gas viscosity at reference temperature |
Required. |
g/cm-s |
PVS0 1.716E-4 | |
Keyword Usage |
Optional. | |||
Reactor Models |
| |||
Reactor Property |
Specify the exponent of the temperature ratio term of the power-law for viscosity. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Exponent of temperature ratio term |
Required. |
-- |
PVSN 0.5 | |
Keyword Usage |
Optional. | |||
Reactor Models |
| |||
Reactor Property |
Specify the reference temperature of the power-law for viscosity. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Reference temperature |
Required. |
K |
PVST 273.15 | |
Keyword Usage |
Optional. | |||
Reactor Models |
| |||
Reactor Property |
The power being supplied to heat the deposition surface or disk. This value is used only if the disk temperature is being calculated from an energy balance by including keyword RADB . See Equation 15–18 of the Chemkin Theory Manual . | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Power |
Required |
cal/(cm 2 ⋅ sec) |
PWRC 15.E7 | |
Keyword Usage |
Optional keyword. By default, the power is 0.0. | |||
Reactor Models |
| |||
Reactor Property |
Total power deposition to the plasma. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Total power deposition |
Required |
Watts |
PWRW 1000. | |
Reactor number (PSR clusters only) |
Optional If no number is given, the value is assumed to apply to all reactors in a cluster. |
-- |
PWRW 1000. 1 | |
Keyword Usage |
Required keyword. | |||
Reactor Models |
| |||
Reactor Property |
The power being supplied to heat the gas as a spatially distributed Gaussian heat source. QDOT is the total power, that is, the spatial integral of the heat source function. See Equation 15–14 of the Chemkin Theory Manual . | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Power |
Required |
erg/(cm 2 ⋅ sec) |
QDOT 1.0E7 | |
Keyword Usage |
Optional keyword. By default, the power is 0.0. | |||
Reactor Models |
| |||
Reactor Property |
The power being supplied to heat the gas as a spatially distributed Gaussian heat source. QDTC is the total power, that is, the spatial integral of the heat source function. See Equation 15–14 of the Chemkin Theory Manual . | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Power |
Required |
cal/(cm 2 ⋅ sec) |
QDTC 1.0E7 | |
Keyword Usage |
Optional keyword. By default, the power is 0.0. | |||
Reactor Models |
| |||
Reactor Property |
Specifies the gas chemistry heat release rate that defines the start of the expansion period. This keyword will take effect only when the gas heat release equation is solved (activated by keyword: QRGEQ ). | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
heat_release_rate |
Required |
cal/sec |
QEXP 0.5 | |
Keyword Usage |
Optional keyword. Default is 0.1 cal/sec. | |||
Reactor Models |
| |||
Reactor Property User Subroutine |
Reactor heat loss will be given as a specified function of time (for 0-D homogeneous reactors) or as a function of distance (for Plug Flow Reactors), through a user-programmed subroutine. FUNCTION PSQFUN (LENIQ, LENRQ, IQFUN, RQFUN) must be provided to specify the heat loss and linked to the application program. See the Application Programming Interface Manual for details on how to work with user subroutines. | |||
Keyword Usage |
Optional keyword. By default, the value there is no heat loss from the reactor. The units returned from the user subroutine must be in erg/sec. See also QPRO. | |||
Reactor Models |
| |||
Notes | ||||
Reactor Property/Model |
The time delay to turn on the droplet temperature equation at the beginning of liquid vaporization to prevent possible convergence issues at the start of injection. When the Droplet Surface T = Core T option is selected, a very large time delay can force the droplet temperature to be constant, that is, equal to the initial liquid temperature, throughout the simulation. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Time |
Required |
seconds |
QIAGE 1.0E-3 | |
Keyword Usage |
Optional keyword. Default is 0.0 sec. | |||
Reactor Models |
| |||
Reactor Property |
The heat loss or heat flux from the reactor to the external environment at an optionally specified surface material. The units are for a total heat loss for 0-D homogeneous reactors, or for heat flux per area for all channel-flow reactors (Plug Flow Reactor, Honeycomb Reactor, Plasma Plug Flow Reactor, and Shear Flow Reactors). This option is only relevant when the energy equation is being solved. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material name (for 0-D homogeneous and plug-flow reactors only) |
Optional If no material is specified, the value will be used for all materials. |
-- |
QLOS material1 50 | |
Bulk name (multiphase reactors only) | Optional | -- | QLOS Gas AMBIENT 0.5 | |
Heat loss or Heat flux (depending on Reactor Model) |
Required |
cal/sec or cal/cm2-s |
QLOS 50 | |
Reactor number (PSR clusters only) |
Optional If no number is given, the keyword is assumed to apply to all reactors in a cluster. |
-- |
QLOS material1 50 1 | |
Keyword Usage |
Optional keyword. By default, there is no heat loss from the reactor. See also QPRO, HTRN, and QFUN. For the multiphase reactors, the keyword is effective for the phase name following the keyword. The name of the bulk phase should be used. "Gas" indicates the gas phase. | |||
Reactor Models |
| |||
Reactor Property Profiles |
This is an additional energy loss term for the electrons that may be introduced to account for inelastic collisional losses that are not already included explicitly in the Gas-phase Kinetics reaction mechanism. Energy loss values are specified here as a function of electron temperature and are given per ionization event to be consistent with the work of Lee, et al.[12] For example, "QLSE 34800. 100." would represent an electron energy loss of 100 eV/ionization event for an electron temperature of 34800 K (3.0 eV). | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Energy loss |
Required |
eV |
QLSE 34800. 100. | |
Electron temperature |
Required |
K |
QLSE 34800. 100. | |
Keyword Usage |
Optional keyword. By default, the additional energy loss term is 0.0. | |||
Reactor Models |
| |||
Reactor Property Profiles |
The heat loss profile or heat flux profile from the reactor to the external environment at an optionally specified surface material, given as a piece-wise linear function of time or distance. Each QPRO entry represents a point in a piecewise-linear profile. The units are for a total heat loss vs. time for 0-D homogeneous reactors, or for heat flux per area vs. distance for all channel-flow reactors (Plug Flow Reactor, Honeycomb Reactor, Plasma Plug Flow Reactor, and Shear Flow Reactors). This option is only relevant when the energy equation is being solved. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Time or Distance value (depending on Reactor Model) |
Required |
sec or cm |
QPRO 1.0E-4 10.0 | |
Heat loss or Heat flux (depending on Reactor Model) |
Required |
cal/sec or cal/cm2-sec |
QPRO 1.0E-4 10.0 | |
Reactor number (PSR clusters only) |
Optional If no number is given, the profile described by the first two values is assumed to apply to all reactors in a cluster. |
-- |
QPRO 1.0E-4 10.0 1 | |
Keyword Usage |
Optional keyword. By default, there is no heat loss from the reactor. See also QLOS, HTRN, and QFUN. | |||
Reactor Models |
| |||
Output |
Solve a separate equation that integrates the heat release due to gas-phase reactions to obtain a more accurate heat-release profile. If this option is not checked, only local heat release rates will be reported at each saved or printed time steps. Only applicable when you are solving the energy equation with transient solver. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Keyword Usage |
Optional keyword. By default, the heat release integration equation is not solved. | |||
Reactor Models |
| |||
Output |
Solve a separate equation that integrates the heat release due to surface reactions to obtain a more accurate heat-release profile. If this option is not checked, only local heat release rates will be reported at each saved or printed time steps. Only applicable when you are solving the energy equation with transient solver. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Keyword Usage |
Optional keyword. By default, the heat release integration equation is not solved. | |||
Reactor Models |
| |||
QXCO Recycling |
This keyword defines the heat-transfer coefficient and the heat-transfer surface area for thermal conductive/convective heat flux between the two specified reactors in a reactor cluster. The direction of the heat flux will come from the higher-temperature reactor to the lower-temperature reactor. This keyword is only relevant when the ENRG keyword is used and when there are multiple reactors in a cluster. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Reactor Number |
Required |
-- |
QXCO 3 6 1.0E-3 1000. | |
Reactor Number |
Required |
-- |
QXCO 3 6 1.0E-3 1000. | |
Heat-transfer coefficient |
Required |
cal/(cm2 ⋅ sec ⋅ K) |
QXCO 3 6 1.0E-3 1000. | |
Heat-transfer surface area |
Required |
cm2 |
QXCO 3 6 1.0E-3 1000. | |
Keyword Usage |
Optional keyword. By default, there is no heat exchange between reactors. | |||
Reactor Models |
| |||
Notes | ||||
QXRA Recycling |
This keyword defines the thermal emissivity/absorptivity and the heat-transfer surface area for thermal radiative flux between the two specified reactors in a reactor cluster. The direction of the heat flux will come from the higher-temperature reactor to the lower-temperature reactor. This keyword is only relevant when the ENRG keyword is used and when there are more than one reactor in a cluster. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Reactor Number |
Required |
-- |
QXRA 2 3 0.1 1000. | |
Reactor Number |
Required |
-- |
QXRA 2 3 0.1 1000. | |
Emissivity/absorptivity |
Required |
-- |
QXRA 2 3 0.1 1000. | |
Heat-transfer surface area |
Required |
cm2 |
QXRA 2 3 0.1 1000. | |
Keyword Usage |
Optional keyword. By default, there is no heat exchange between reactors. Note that the order of the two reactor numbers that define the heat connection is un-important. | |||
Reactor Models |
| |||
Notes | ||||
Reactor Property |
By default, when the gas-phase thermal radiation calculation is on, contributions from all major radiating species (such as CO2, H2 O, CO, and CH4) will not be included. A major radiating species is a species of which the absorption coefficient is available to the application. This keyword allows the user to include the contribution of a major species in the radiation heat loss calculation. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Species symbol |
Required |
-- |
RACTV CO | |
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Reactor Property |
Use an energy balance to determine the disk or susceptor (deposition surface) temperature. If RADB is specified, TDSK is used as the initial guess for the susceptor temperature. | |||
Keyword Usage |
Optional keyword. By default, the susceptor temperature is fixed as TDSK. | |||
Reactor Models |
| |||
Reactor Property |
Turns on the radiation heat loss term in the gas energy equation. The optional model number indicates which thermal radiation model will be employed to calculate the radiation intensity. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Reactor number |
Required |
-- |
RADGS 0 | |
Keyword Usage |
Currently, the optically-thin limit model is the only model implemented and hence is the default model. The model number for the optically-thin limit model is 0. | |||
Reactor Models |
| |||
Reactor Property |
Allows radiative heat loss contribution from particulates associated with the named material to be included independently. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Material Name |
Required |
-- |
RADPT CO | |
Reactor Models |
| |||
Solver |
Maximum relative change in the surface site fractions (over one time step) for which the initial fictitious transient equations that establish the initial surface site fractions can be considered to have converged to steady state. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Maximum relative change |
Required |
-- |
RCHG 1.0E-3 | |
Keyword Usage |
Optional keyword. By default, the maximum relative change is set to 1.0E-6. | |||
Reactor Models |
| |||
Reactor Property |
Ratio of the substrate radius to the separation distance between it and the upper radiating disk. This is used in calculating a surface radiation balance. RRAD is used only if the disk temperature is being calculated by including keyword RADB . See Equation 15–18 of the Chemkin Theory Manual . | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Ratio of substrate |
Required |
-- |
RDSK 3.0 | |
Keyword Usage |
Optional keyword. This is keyword is required only when RRAD and RADB are included. | |||
Reactor Models |
| |||
Inlet or Reactor Property |
Mole fraction of the reagent gases entering the reactor for an inlet stream or for the initial conditions in a closed system. For example, REAC fuel1 C2H2 0.5, would indicate that acetylene has a mole fraction of 0.5 in the inlet stream named fuel1. The sum of all the reactant mole fractions should equal to one. However, if they do not the fractions will be normalized so that they do sum to one, and a warning message will be printed to the output file. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Inlet stream name (for PSRs and CVD Reactors only) |
Optional If there is no stream name than the reactant and mole fraction apply to all streams. |
-- |
REAC fuel1 C2H2 0.5 | |
Species name |
Required |
-- |
REAC C2H2 0.5 | |
Reactant fraction |
Required |
mole fractions |
REAC C2H2 0.5 | |
Keyword Usage |
Required keyword, except in cases where an equivalence ratio option is used ( EQUI). | |||
Reactor Models |
| |||
Notes | ||||
Recycling |
For a cluster of reactors (NPSR > 1), specifies recycling or routing of a mass flow from one reactor to another and the fractional flow associated with this stream. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Reactor Number, from which the flow originates |
Required |
-- |
RECY 2 1 0.3 | |
Reactor Number, to which the flow is transferred |
Required |
-- |
RECY 2 1 0.3 | |
Percent that will be recycled from Reactor 2 back into Reactor 1 |
Required |
-- |
RECY 2 1 0.3 | |
Keyword Usage |
Optional keyword. By default all flow out of a reactor in will flow into the next reactor in the series (e.g. RECY 1 2 1.0 and RECY 2 3 1.0 for a three-reactor system). If recycle loops are defined, then the effective "recycling" from the upstream into the downstream reactor will be one minus the sum of the recycle streams out of the upstream reactor into other reactors. | |||
Reactor Models |
| |||
Solver |
Controls the convergence method used for transient runs. When applied, it uses a relaxed scheme whereby the integrator solver tries harder to achieve a solution at each time, but occasionally may result in increased time to solve your problem or numerical instabilities. Therefore, you should use this only if your transient run fails with a "nonlinear solver failed to converge repeatedly" message or you believe your problem is very stiff, highly nonlinear or discontinuous. | |||
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Solver |
This keyword is used to override the default value for the relative perturbation in the solution variable used in the determination of the numerically derived Jacobian. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Relative perturbation |
Required |
-- |
RELT 1.E-15 | |
Keyword Usage |
Optional keyword. By default, the relative perturbation is set equal to the square root of the unit round-off error of the machine. | |||
Reactor Models |
| |||
Reactor Property |
The option may be used when the TRCE option is in effect. Using TRCE, the conservation equation for the last species in the gas-phase and each surface and bulk phase is not solved: the last species concentration (mass fraction or site fraction) is chosen so that the fractions sum to one. The REOR option causes TRCE to choose dynamically and locally (at each mesh point and in each phase) the species of largest concentration and not solve its conservation equation. | |||
Keyword Usage |
Optional keyword. By default, the last species in each phase is chosen. | |||
Reactor Models |
| |||
Reactor Property |
Mass density before the incident shock. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Mass density |
Required |
gm/cm 3 |
RHO1 1.E-4 | |
Keyword Usage |
Optional keyword. The shock velocity and any two of temperature, pressure, or density must be specified for conditions before the incident shock. See also T1 and P1A . | |||
Reactor Models |
| |||
Reactor Property |
Mass density after the incident shock. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Mass density |
Required |
g/cm 3 |
RHO2 1.E-4 | |
Keyword Usage |
Optional keyword. Any two of temperature, pressure, or density must be specified for conditions after the incident shock. See also T2 and P2A . | |||
Reactor Models |
| |||
Reactor Property |
Mass density after the reflected shock. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Mass density |
Required |
g/cm 3 |
RHO3 1.E-4 | |
Keyword Usage |
Optional keyword. Any two of temperature, pressure, or density must be specified for conditions after the reflected shock. See also T3 and P3A . | |||
Reactor Models |
| |||
Reactor Property |
This optional keyword is used to turn the real gas model on or off. Setting the option value to 1 will activate the real gas model if the gas reaction mechanism contains the real gas data. A value of 0 = turn OFF the real gas model and 1= turn ON the model. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Enabled |
Required |
g/cm 3 |
RLGAS 1 | |
Keyword Usage |
Optional keyword. By default, the real gas model is turned OFF. | |||
Reactor Models |
| |||
Reactor Property |
This optional keyword will activate the selected real gas mixing rule if the real gas model is turned on (by RLGAS). A value of 0 = use the Van der Waals mixing rule and 1 = use the pseudocritical method (see Real Gas Data). | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Method |
Required |
None |
RLMIX 0 | |
Keyword Usage |
Optional keyword. By default, the van der Waals method will be applied. | |||
Reactor Models |
| |||
Output |
Inclusion of this keyword causes the rate-of-production coefficients to be printed for specified species. The keyword must be followed by one or more names of species. If any ROP keywords are used, all the rate-of-production coefficients will be computed and written to the XML Solution File (for example, XMLdata.zip). However, only those specified by the ROP keyword will be printed in the diagnostic output file. More than one species may be entered per line. If the line is blank after the ROP keyword, then all rate-of-production contributions are computed and written to the XML Solution File, but none are printed. | |||
Keyword Usage |
Optional keyword. By default, no rate-of-production values are computed. | |||
Reactor Models |
| |||
Notes |
| |||
Reactor Property |
Revolutions per minute of the engine crank arm. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Revolutions per minute |
Required |
rpm |
RPM 1200 | |
Keyword Usage |
Optional keyword. By default, the rpm is 1500. | |||
Reactor Models |
| |||
Reactor Property |
Ratio of the upper radiating disk radius to the separation distance between it and the lower substrate. This is used in calculating a surface radiation balance. RRAD is used only if the disk temperature is being calculated by including keyword RADB . See Equation 15–18 of the Chemkin Theory Manual . | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Ratio of the upper radiating disk |
Required |
-- |
RRAD 3.0 | |
Keyword Usage | ||||
Reactor Models |
| |||
Problem Type |
Inclusion of this keyword designates a reflected shock problem. | |||
Keyword Usage |
Required keyword. See also ISHK. | |||
Reactor Models |
| |||
Cluster Property |
Inclusion of this keyword causes Ansys Chemkin to read a solution off the XML Solution File (for example, XMLdata.zip) and begin iteration or integration on the current reactor conditions from this solution. | |||
Keyword Usage |
Optional keyword. By default, a solution is started from the user-specified conditions and no XML Solution File is used. | |||
Reactor Models |
| |||
Solver |
Relative tolerance for convergence of Newton iteration as it is used in the pseudo time stepping procedure for steady-state problems employing the Twopnt solver. Since we are not seeking accuracy in a transient solution, this convergence criteria typically does not need to be as stringent as for the Newton iteration on the actual steady-state solution. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Absolute tolerance |
Required |
-- |
RTIM 1.E-3 | |
Keyword Usage |
Optional keyword. By default, the relative tolerance is 1.E-4. See also ATIM. | |||
Reactor Models |
| |||
Notes |
| |||
Reactor Property |
Turn on or off solution of the residence-time equation for a plug-flow simulation. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
String "ON" or "OFF" to toggle the momentum equation |
Required |
-- |
RTIME ON RTIME OFF | |
Keyword Usage |
Optional keyword. By default, the residence-time equation is solved (ON). | |||
Reactor Models |
| |||
Solver |
A different relative tolerance can be assigned to moment variables in steady-state calculations. By default, the same relative tolerance given by RTOL is used for all variables. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Tolerance |
Required |
-- |
RTLM 1.0E-4 | |
Keyword Usage |
Optional keyword. By default, the absolute tolerance is determined by RTOL. | |||
Reactor Models |
| |||
Solver |
Relative tolerance used by the transient solver, DASPK, as an indicator of the accuracy desired in the solution for the sensitivity coefficients only. Generally, the sensitivity coefficients need not be solved to a great degree of accuracy, so these tolerances should be lower than the tolerances placed on the physical variables. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Relative tolerance |
Required |
-- |
RTLS 1.E-2 | |
Keyword Usage |
Optional keyword. By default, the relative tolerance is 1.E-5. | |||
Reactor Models |
| |||
Solver |
Relative tolerance used by the solver to determine convergence and as an indicator of the accuracy desired in the physical solution. In general the value of RTOL roughly corresponds to the number of significant digits that should be expected from a solution. A typical value should be between 10-3 and 10-6, which would provide roughly three to six significant digits. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Relative tolerance |
Required |
-- |
RTOL 1.E-3 | |
Keyword Usage |
Optional keyword. The default values are: Open 0-D Reactors run in steady-state mode, Opposed-flow Flame, Premixed Laminar Burner-stabilized Flame, Premixed Laminar Flame-speed Calculation, Shear Flow Reactor: 1.E-4 Normal Incident Shock, Normal Reflected Shock, Plug Flow Reactor, Partially Stirred Reactor (PaSR), CVD: 1.E-6 Closed 0-D Reactors and Open 0-D Reactors run in transient mode: 1.E-8 See also ATOL. | |||
Reactor Models |
| |||
Output |
Request the scatter plot of a scalar to be output to the file scatter.plt. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Scalar (temperature or species name) |
Required |
-- |
SCAT CH4 | |
Keyword Usage |
Optional keyword. By default, no scatter plot is printed. | |||
Reactor Models |
| |||
Inlet Property |
The volumetric flow rate into the reactor for an optionally specified inlet stream, in standard cubic centimeters per minute assuming that the inlet temperature is 298.15 K and the inlet pressure is 1 atm unless a different value for TSCCM is provided. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Inlet stream name |
Optional If there is no stream name than the volumetric flow rate applies to the default or all defined streams. |
-- |
SCCM secondary_air 300 | |
Equivalent volumetric flow rate at standard conditions |
Required |
standard cm 3 /min |
SCCM secondary_air 300 | |
Keyword Usage |
PSRs and PaSRs: Optional keyword. If none of TAU, FLRT / FPRO, SCCM / SCCMPRO are specified or are nonzero, then a closed-system is assumed. FLRT / FPRO or SCCM / SCCMPRO is required for each INLET stream defined. Stagnation Flow CVD Reactors: FLRT / FPRO or SCCM / SCCMPRO or UINL is required for each inlet stream defined. Rotating Disk CVD Reactors: Optional keyword. | |||
Reactor Models |
| |||
Inlet Property Profiles |
Used to specify a transient profile or function of mass flow rate vs. time for an inlet stream, in standard cubic centimeters per minute assuming that the inlet temperature is 298.15 K and the inlet pressure is 1 atm unless a different standard temperature ( TSCCM) is entered. The profile specified will be interpolated linearly from the SCCMPRO points provided. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Inlet stream name |
Optional If no stream name is given, the profile described by the reactant and mole fraction is assumed to apply to all reactors in a cluster. |
-- |
SCCMPRO purge 0.19 300 | |
Time |
Required |
sec (cm for flow reactors) |
SCCMPRO 0.19 300 | |
Equivalent volumetric flow rate at standard conditions |
Required |
standard cm 3 /min |
SCCMPRO 0.19 300 | |
Keyword Usage |
PFRs and Monolith Reactors: Flow specification via one of VEL, VDOT, VDOTPRO SCCM SCCMPRO FLRT, or FPRO is required. PSRs and PaSRs: Optional keyword. If none of TAU, FLRT / FPRO, SCCM / SCCMPRO are specified or are nonzero, then a closed-system is assumed. FLRT / FPRO or SCCM / SCCMPRO is required for each INLET stream defined. Stagnation Flow CVD Reactors: FLRT / FPRO or SCCM / SCCMPRO or UINL is required for each inlet stream defined. Rotating Disk CVD Reactors: Optional keyword. | |||
Reactor Models |
| |||
Reactor Property |
Scaling factor for the particles moments (moments method) or number density (sectional method). A non-unity value for this parameter changes the units of the (internal) solution variable for particle moments or number density. For example, setting it to 1.0E+06 results in micro-moles whereas setting it to 1.0E+09 means that it is nano-moles. A value of 1 would mean that the unit should be moles. A recommended value for typical problems is 1.0E+12. Such scaling helps preserve the positivity of the solution during numerical computation. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Scaling factor |
Required |
-- |
SCLM 1.0E+12 | |
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Reactor Property |
Scaling factor for the particle surface species concentrations. A non-unity value for this parameter changes the units of the (internal) solution variable for particle surface species. For example, setting it to 1.0E+06 results in micro-moles whereas setting it to 1.0E+09 means that it is nano-moles. A value of 1 would mean that the unit should be moles. A recommended value for typical problems is 1.0E+12. Such scaling helps preserve the positivity of the solution during numerical computation. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Scaling factor |
Required |
-- |
SCLS 1.0E+12 | |
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Solver |
Flag instructing that the transient solver, DASPK will use staggered corrector method to solve sensitivity equations. The staggered corrector method is the sensitivity method that was used in previous versions of Ansys Chemkin and is mainly provided for backwards compatibility. It is generally slower than the default sensitivity method in Chemkin (which is the staggered direct method) but sometimes can be more stable and robust than the staggered direct method. | |||
Keyword Usage |
Optional keyword. By default, DASPK uses staggered corrector method to solve sensitivity equations. | |||
Reactor Models |
| |||
Notes |
| |||
Output |
Analyze the coverage dependence of a surface reaction, that is, create a table of effective reaction rates versus temperature. Surface coverage is assumed to be that of the bath-gas composition. The ALL option is the default and produces tables for every surface reaction. The NONE option suppresses output for all of the reactions. If reaction information is desired for only certain reactions, they may be optionally specified by their number (given in the Pre-processor output) or by typing an exact duplicate of the reaction expression (see example input). | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
ALL option |
Optional, default is ALL |
-- |
SCOV ALL | |
NONE option |
Optional, default is ALL |
-- |
SCOV NONE | |
Surface reaction number list |
Optional, default is ALL |
-- |
SCOV 2 5 | |
Surface reaction expression |
Optional, default is ALL |
-- |
SCOV CH(S)+H<=>C(S,R)+H2 | |
Keyword Usage |
Optional keyword. By default, the table output is determined by the ALL or NONE keyword. | |||
Reactor Models |
| |||
Output |
Write output data to a standard (ascii) print-out file. | |||
Keyword Usage |
Optional keyword. By default, solution data will be written to an ascii output file. | |||
Reactor Models |
| |||
Output |
Inclusion of this keyword causes the calculation of the first-order sensitivity coefficients, with respect to the gas-phase and surface chemistry rate constants, for the growth rate of all bulk phases. Growth-rate sensitivities will be included in the printed output and the XML Solution File (for example, XMLdata.zip). | |||
Keyword Usage |
Optional keyword. By default, no sensitivity coefficients are computed. See also ASEN. | |||
Reactor Models |
| |||
Notes |
| |||
Output |
Calculate and store sensitivity coefficients for gas temperature with respect to reaction A-factors. See ASEN. | |||
Keyword Usage |
Optional keyword. By default, no sensitivity coefficients are computed or printed. Same as ASEN TEMP. | |||
Reactor Models |
| |||
Reactor Property |
This keyword specifies that the rates of all surface reactions will be multiplied (scaled) by the factor SFAC. This option is sometimes useful if convergence difficulties are encountered due to unusually large reaction rates. The problem would be first solved with artificially reduced reaction rates, which then can be increased in subsequent continuations or restarts until SFAC is one. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Multiplier value |
Required |
-- |
SFAC 2.0 | |
Reactor number (PSR clusters only) |
Optional If no number is given, value is assumed to apply to all reactors in a cluster. |
-- |
SFAC 2.0 1 | |
Keyword Usage |
Optional keyword. By default, the multiplier value is set to 1.0. | |||
Reactor Models |
| |||
Solver |
Sometimes during the solution procedure some of the very small gas-phase mass fractions, surface site fractions, or bulk species fractions may be calculated as a slightly negative number. No solution component will be allowed to drop below the floor value specified by SFLR. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Minimum bounds on the solution variables |
Required |
-- |
SFLR -1.E-5 | |
Keyword Usage |
Optional keyword. By default, the minimum bounds on the solution variables is set to -1.E-4 | |||
Reactor Models |
| |||
Solver |
Set the minimum bounds of the surface species concentration to a slightly negative number to allow the solver more room to search for a solution. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Minimum bound |
Required |
-- |
SFMN -1.0d-06 | |
Keyword Usage |
Optional keyword. Usable only with Particle Tracking. | |||
Reactor Models |
| |||
Solver |
This controls the maximum number of iterations the segregated solver can take per step to solve the problem. The default is 100 and you may increase this value to give the solver greater chance to solve your problem if it is very hard to solve. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Scaling factor |
Required |
-- |
SGMAXIT 100 | |
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Solver |
Absolute tolerance criterion on gas-phase mole fractions in segregated scheme. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Absolute tolerance |
Required |
-- |
SGTOL 1.0E-10 | |
Keyword Usage |
Optional keyword. The default value is 1E-10. | |||
Reactor Models |
| |||
Solver |
Turns on the multi-zone SI Engine Zonal simulation with gas-phase chemistry de-activated. The number of zones is set to 2 by default. SIKN and SIDR are mutually exclusive. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Number of zones |
Required |
-- |
SIDR 2 | |
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Solver |
Turns on the multi-zone SI Engine Zonal simulation with gas-phase chemistry activated. The number of zones is set to 2 by default.SIKN and SIDR are mutually exclusive. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Number of zones |
Required |
-- |
SIKN 2 | |
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Reactor Property |
Specifies the crank angle when the SI Engine Zonal Simulator properties will be saved to the XML solution file. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
crank_angle |
Required |
degree |
SIOA 5.1 | |
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Output |
Use this keyword to set the data block size in bytes for the XML Solution File (for example, XMLdata.zip). Changing this value may affect the performance of the XML parsing routines in the graphical Ansys Chemkin Post-processor. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Data block size |
Required |
bytes |
SIZE 10000000 | |
Keyword Usage |
Optional keyword. By default, the data block size is 10 MB. | |||
Reactor Models |
| |||
Reactor Property |
Use the slip velocity model to calculate axial velocity at wall when Knudsen number is large. The model calculates the axial velocity at wall as where is the characteristic length, is the axial velocity, is the multiplier, is the tangential momentum accommodation coefficient. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Multiplier |
Required |
-- |
SLIP 3.0 0.9 | |
Tangential momentum accommodation coefficient |
Required |
-- |
SLIP 3.0 0.9 | |
Keyword Usage |
Optional keyword. By default, the slip velocity model is not used. | |||
Reactor Models |
| |||
_TECHNIQUE Solver |
Controls the underlying solution technique. Previous versions of Ansys Chemkin use an older and generally less robust solution method. By default, solution_technique is set to 1, which means the new and generally more robust (and for larger mechanisms often faster) technique is used. Setting solution_technique to 0 uses the older method and you should only use this if you are having convergence issues with Chemkin and are confident you do not have any problems with your mechanism or problem specification. | |||
Keyword Usage |
Optional keyword. By default, SOLUTION_TECHNIQUE is set to 1. | |||
Reactor Models |
| |||
Problem Type |
Constant pressure and entropy constraints. | |||
Keyword Usage |
Optional keyword. Exactly one problem-type keyword must be included. | |||
Reactor Models |
| |||
Notes |
| |||
Solver |
This keyword provides a (small positive) number that will replace any negative species mass or site fractions. The replacement is made after every successful sequence of time steps, upon adding mesh points, and on restart or continuation. SPOS is often helpful in starting difficult problems when the initial guess is far from the solution. SPOS attempts to force the transient solution away from nonphysical regions that may otherwise be entered due to bad initial conditions and badly conditioned systems. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Species mass fraction |
Required |
-- |
SPOS 1.E-14 | |
Keyword Usage |
Optional keyword. By default, no substitution is made for negative fractions during solution for all Reactor Models except for Opposed-flow Flames, where the default value is 1.E-10. | |||
Reactor Models |
| |||
Solver |
A pseudo wall thermal conductivity to allow surface enthalpy production to "overflow" in the downstream direction. This keyword is useful when the reactor model fails to converge repeatedly because of stiff surface chemistry and the reactor wall temperature is not fixed. The overall enthalpy of the reactor is still conserved because this pseudo wall enthalpy flux is included in the energy equation. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Pseudo conductivity |
Required |
-- |
SQRX 0.001 | |
Keyword Usage |
Optional keyword. By default, no thermal conduction in wall is considered. | |||
Reactor Models |
| |||
Output |
Prints out a table of reaction rates and other pertinent information for a surface reaction. The ALL option is the default and produces tables for every surface reaction. The NONE option suppresses output for all of the reactions. If reaction information is desired for only certain reactions, they may be optionally specified by their number (given in the Pre-processor output) or by typing an exact duplicate of the reaction expression (see example input). | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
ALL option |
Optional, default is ALL |
-- |
SRXN ALL | |
NONE option |
Optional, default is ALL |
-- |
SRXN NONE | |
Surface reaction number list |
Optional, default is ALL |
-- |
SRXN 2 5 | |
Surface reaction expression |
Optional, default is ALL |
-- |
SRXN CH(S)+H<=>C(S,R)+H2 | |
Keyword Usage |
Optional keyword. By default, the table output is determined by the ALL or NONE keyword. | |||
Reactor Models |
| |||
Reactor Property |
The nominal value of the Stoichiometric Scalar Dissipation Rate (SSDR). The first flamelet will be computed for this value. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Nominal value of SSDR |
Required |
1/s |
SSDR 1.0 | |
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Reactor Property |
The maximum value of the Stoichiometric Scalar Dissipation Rate (SSDR). After computing a flamelet for the nominal value (specified by keyword SSDR), continuations to SSDR_MAX are done in a number of steps as specified by keyword NSTEP_HIGH. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Maximum value of SSDR |
Optional |
1/s |
SSDR_MAX 100 | |
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Reactor Property |
The minimum value of the Stoichiometric Scalar Dissipation Rate (SSDR). After computing a flamelet for the nominal value (specified by keyword SSDR), continuations to SSDR_MIN are done in a number of steps as specified by keyword NSTEP_LOW. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Minimum value of SSDR |
Optional |
1/s |
SSDR_MIN 0.001 | |
Keyword Usage |
Optional keyword. | |||
Reactor Models |
| |||
Solver |
Skip the initial surface site fraction calculation. | |||
Keyword Usage |
Optional keyword. By default, an initial solution is performed to determine the surface site fractions holding the reagent gas species constant. | |||
Reactor Models |
| |||
Solver |
The maximum number of iterations per steady state search, in the steady-state solver TWOPNT. This is the maximum number of iterations that are allowed each time TWOPNT searches to find the steady state solution. Typically you will not need to change this maximum because TWOPNT will revert to its time stepping algorithm and then re-try searching for the steady state. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Maximum steady state iterations |
Optional |
-- |
SSMAXITER 120 | |
Keyword Usage |
Optional keyword. By default, the maximum number of iterations is 100. | |||
Reactor Models |
| |||
Notes |
| |||
Solver |
A pseudo diffusivity for surface species to allow them to diffuse along the wall surface in the downstream direction. This keyword is useful when the reactor model fails to converge repeatedly because of stiff surface chemistry and the reactor wall temperature is fixed. The overall mass and element conservations of the reactor are still satisfied because pseudo surface species fluxes are included in the surface species equations. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Pseudo conductivity |
Required |
-- |
SSRX 0.0001 | |
Keyword Usage |
Optional keyword. By default, no surface species flux on wall is considered. | |||
Reactor Models |
| |||
Notes |
| |||
Solver |
Inclusion of this keyword indicates that the local sensitivity analysis will be performed instead of the integrated sensitivity analysis for transient or plug-flow calculations. This may be helpful in speeding up calculations of sensitivity, but we caution that the local sensitivity is less accurate than the integrated sensitivity. | |||
Keyword Usage |
Optional keyword. By default, the integrated sensitivity analysis will be performed for transient calculations when sensitivity data is requested. | |||
Reactor Models |
| |||
Notes |
| |||
Problem Type |
Specify a Stagnation Flow CVD Reactor model. | |||
Keyword Usage |
Required keyword. See also OMEG. If the keyword STAG is given and the spin rate OMEG is nonzero, then this inconsistent input will generate an error. A stagnation-point flow can also be specified by using "OMEG 0". | |||
Reactor Models |
| |||
_FLAME Problem Type |
Indicates Burner-stabilized Stagnation Flow problem type. | |||
Keyword Usage |
Required keyword. | |||
Reactor Models |
| |||
Reactor Property |
Parameter to produce a non-uniform grid. For cartesian coordinates the initial grid location for a node J is X(J)=A*(J-1)**STCH, where A=HITE/(NPTS-1)**STCH, HITE is the reactor height, and NPTS is the total number of grid nodes. If STCH=1, a uniform grid is produced. For STCH > 1, the grid is more tightly spaced at the lower boundary (cartesian-coordinates) or at the outer boundary ( cylindrical coordinates), and consequently the grid is more widely spaced at the other boundary. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Cartesian coordinates |
Required |
-- |
STCH 1.2 | |
Keyword Usage |
Optional keyword. By default, the program is set to 1. | |||
Reactor Models |
| |||
Output |
Analyzes the forward and reverse surface reaction’s sticking coefficient, if applicable. The ALL option is the default and produces tables for every surface reaction with a sticking-coefficient formulation. The NONE option suppresses output for all of the reactions. If reaction information is desired for only certain reactions, they may be optionally specified by their number (given in the Pre-processor output) or by typing an exact duplicate of the reaction expression (see example input). | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
ALL option |
Optional, default is ALL |
-- |
STCK ALL | |
NONE option |
Optional, default is ALL |
-- |
STCK NONE | |
Surface reaction number list |
Optional, default is ALL |
-- |
STCK 2 5 | |
Surface reaction expression |
Optional, default is ALL |
-- |
STCK CH(S)+H<=>C(S,R)+H2 | |
Keyword Usage |
Optional keyword. By default, the table output is determined by the ALL or NONE keyword. | |||
Reactor Models |
| |||
Solver |
Initial time step size used by the steady-state solver Twopnt during the initial calculation for the surface conditions at the inlet. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Initial time step |
Required |
cm |
STP0 1.0E-7 | |
Keyword Usage |
Optional keyword. By default, the initial time step is 1.0E-6. | |||
Reactor Models |
| |||
Solver |
The maximum internal time step for the solver in transient calculations. STPT determines the largest time-step the transient solver can take at one time and thereby controls the resolution for interpolation of specified time-profiles. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Time step |
Required |
sec |
STPT 1.0E-4 | |
Aurora Usage |
Optional keyword. If not specified, then If either DELT or DTSV are specified, STPT is set to the smallest of these values. If neither DELT nor DTSV are specified, then STPT is set to the value of the end time divided by 100. | |||
Reactor Models |
| |||
Notes | ||||
Reactor Property |
The solution will be obtained using a steady-state calculation (with the solver Twopnt) rather than a transient calculation (using the solver DASPK). | |||
Keyword Usage |
Optional keyword. By default, a steady-state calculation is performed. | |||
Reactor Models |
| |||
Notes |
| |||
Reactor Property |
Initial values (transient) or estimates (steady-state) for the surface site fraction values for the surface species on each surface site type (surface phase). | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Surface species name |
Required |
-- |
SURF Ga(s) 0.001 | |
Surface fractions |
Required |
site fractions |
SURF Ga(s) 0.001 | |
Keyword Usage |
Optional keyword. By default, the initial or estimated surface-site fractions are 0.0. | |||
Reactor Models |
| |||
Notes |
| |||
Reactor Property |
Specify the reference gas viscosity at the reference temperature of the Sutherland's-law for viscosity. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Reference gas viscosity at reference temperature |
Required. |
g/cm-s |
SVS0 1.716E-4 | |
Keyword Usage |
Optional. | |||
Reactor Models |
| |||
Reactor Property |
Specify the Sutherland temperature of the Sutherland's-law for viscosity. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Sutherland temperature |
Required. | K |
SVSS 114.0 | |
Keyword Usage |
Optional. | |||
Reactor Models |
| |||
Reactor Property |
Specify the reference temperature of the Sutherland's-law for viscosity. | |||
Parameters |
Optional/Reqd. |
Units |
Examples | |
Reference temperature |
Required. |
K |
SVST 273.15 | |
Keyword Usage |
Optional. | |||
Reactor Models |
| |||
Reactor Property |
Keyword for temperature boundary condition on the upper wall (only used for non-symmetric cartesian coordinates). The upper wall temperature is set equal to the bottom wall temperature if SYMT is specified. | |||
Keyword Usage |
Optional keyword. By default, an adiabatic top wall is used. | |||
Reactor Models |
|