@@ -6,8 +6,8 @@ In practise, DART is initialized by using a dictionary of parameters, and the ty
...
@@ -6,8 +6,8 @@ In practise, DART is initialized by using a dictionary of parameters, and the ty
```python
```python
cfg={
cfg={
# Options
# Options
'Threads':int,# number of threads
'Threads':int,# number of threads (optional, default=1)
'Verb':int,# verbosity
'Verb':int,# verbosity (optional, default=1)
# Model (geometry or mesh)
# Model (geometry or mesh)
'File':str,# Input file containing the model
'File':str,# Input file containing the model
'Pars':dict,# parameters for input file model
'Pars':dict,# parameters for input file model
...
@@ -30,7 +30,7 @@ cfg = {
...
@@ -30,7 +30,7 @@ cfg = {
'Fuselage':str,# name of physical group containing the fuselage boundary
'Fuselage':str,# name of physical group containing the fuselage boundary
'WakeExs':str,# LIST of names of physical group containing the free edge of the wake and the intersection of lifting surface with fuselage (to be excluded from Wake B.C.), only required if a 'Fuselage' if present, otherwise 'WakeTips' is sufficient
'WakeExs':str,# LIST of names of physical group containing the free edge of the wake and the intersection of lifting surface with fuselage (to be excluded from Wake B.C.), only required if a 'Fuselage' if present, otherwise 'WakeTips' is sufficient
# Freestream
# Freestream
'M_inf':float,# freestream Mach number
'M_inf':float,# freestream Mach number (optional, default=0)
'AoA':float,# freestream angle of attack [deg] (optional, default=0)
'AoA':float,# freestream angle of attack [deg] (optional, default=0)
'AoS':float,# freestream angle of sideslip [deg] (optional, default=0)
'AoS':float,# freestream angle of sideslip [deg] (optional, default=0)
'Q_inf':float,# freesteam dynamic pressure (only required for aerostructural computations)
'Q_inf':float,# freesteam dynamic pressure (only required for aerostructural computations)