The configuration file
The .conf file contains different options which specify the problem that APM will solve. The contents of an example .conf file are shown below:
The values in the above .conf file are in SI units - m, kg, s. You can use different units as long as they are consistent across the .conf file.
Refer to the table below for a detailed description of each option.
Option
Dimensionality
Description
Default value
c_ref
Reference chord, used for non-dimensionalisation of the aerodynamic coefficients
1
b_ref
Reference span, used for non-dimensionalisation of the aerodynamic coefficients
1
S_ref
Reference area, used for non-dimensionalisation of the aerodynamic coefficients
1
x_cg, y_cg, z_cg
Location of the centre of gravity
0
trailing_edge_angle
-
Edges sharper than the trailing edge angle in degrees are identified as trailing edges
150
p_ref
Reference pressure
101325
rho_ref
Reference density
1.225
mu_ref
Reference dynamic viscosity
1.789e-5
norm_V_ref
Reference freestream speed
1
M_ref
-
Reference Mach number (used for compressibility corrections)
0
alpha, beta
-
Angle of attack and angle of sideslip with respect to the freestream in degrees
0
p, q, r
Roll, pitch, and yaw rates in degrees/sec
0
dt
Time step
1
N_timesteps
-
Number of timesteps
1
restart_from_checkpoint
-
Instructs the solver to restart the solution from a checkpoint
0
wake_alignment, wake_angle
-
Specifies how the wake aligns with respect to the trailing edges
0
wake_rollup
-
If disabled the induced velocities from the body on the wake and on the wake iteslf wont be calculated. The wake will be translated with the reference freestream speed.
1
json_output, paraview_output, tecplot_output
-
Enables or disables JSON, ParaView, and Tecplot output
0
extended_output
-
Appends force and moment vector for each panel in the Paraview and Tecplot output files
0
doublet_gradient_scheme
-
0
neighbour_tolerance
-
Specifies the neighbour tolerance criteria
1e-6
tip_panels
-
Instructs the solver to label specific panels as type 6
Empty
symmetry
-
Enables symmetry across the x-y plane. The solutions 2x faster and the memory requirements are 2x lower.
0
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