Tethered Wing data extraction

[aweproject2023]

i am wondering how I can extract raw data (text or cvs) of these plots generated from tethered wing example?

[aweproject2023]

The following script works for me for wing-example case raw data extraction. But for tethered wing case in circular path, I am wondering is it possible to extract wing loading for every half circle? Thx!

#push!(CLs, CL)
#push!(CDs, CD)

#push!(rolls, roll)
#push!(pitchs, pitch)
#push!(yaws, yaw)

push!(spanposs, spanpos)
push!(ls, l)
push!(ds, d)

f = open("rawdata_lift.txt", "w")
println(f, ls)
close(f)

f = open("rawdata_span.txt", "w")
println(f, spanposs)
close(f)

[EdoAlvarezR]

Similar to this thread: LINK

In order to determine the half circle I'd suggest applying some logic based on the current step number.