Repository containing the files for the thesis : Optimization of an aircraft design problem for hybrid-electric configurations under manufacturing and certification constraints
Implemented a surrogate model for the estimation of the turboshaft performances based on the original model. One of the moel in the computation of the slipstream for the turboshaft requires him to be connected to a variable from the performances. Implemented a first version of a mechanism that allows to do that. Still to be improved because data coming from the mission are 92 long while for slipstream its only 90.
Also added some correction to models with wrong units and extended modeling capabilties.
TBM900 and Kodiak 100 are now reference cases for this framework
Implemented a surrogate model for the estimation of the turboshaft performances based on the original model. One of the moel in the computation of the slipstream for the turboshaft requires him to be connected to a variable from the performances. Implemented a first version of a mechanism that allows to do that. Still to be improved because data coming from the mission are 92 long while for slipstream its only 90. Also added some correction to models with wrong units and extended modeling capabilties. TBM900 and Kodiak 100 are now reference cases for this framework