Repository containing the files for the thesis : Optimization of an aircraft design problem for hybrid-electric configurations under manufacturing and certification constraints
GNU General Public License v3.0
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Verification of propeller's ability to generate thrust #43
Added a small mechanic that checks that the propeller is connected to a source so that it can indeed generate thrust. When it is not connected to a source, it's contribution is forced to 0
Added a small mechanic that checks that the propeller is connected to a source so that it can indeed generate thrust. When it is not connected to a source, it's contribution is forced to 0