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The fan pressure ratio in the optimization tutorial (example_opt.jl) only gets updated as ac.pare[iepif, ipclimbn, :] .= x[13] #Fan PR
However, the design fan pressure ratio is that at the start of cruise, ipcruise1. The above line means that the variable does not have an impact on the aircraft.
The text was updated successfully, but these errors were encountered:
The fan pressure ratio in the optimization tutorial (example_opt.jl) only gets updated as
ac.pare[iepif, ipclimbn, :] .= x[13] #Fan PR
However, the design fan pressure ratio is that at the start of cruise,
ipcruise1
. The above line means that the variable does not have an impact on the aircraft.The text was updated successfully, but these errors were encountered: