AeroForcesCalculator¶
Calculates the total aerodynamic forces on the frame of reference
A
.The settings that this solver accepts are given by a dictionary, with the following key-value pairs:
Name Type Description Default folder
str
Output folder location ./output
write_text_file
bool
Write txt
file with resultsFalse
text_file_name
str
Text file name screen_output
bool
Show results on screen True
unsteady
bool
Include unsteady contributions False
coefficients
bool
Calculate aerodynamic coefficients False
q_ref
float
Reference dynamic pressure 1
S_ref
float
Reference area 1