Repository containing the files for the thesis : Optimization of an aircraft design problem for hybrid-electric configurations under manufacturing and certification constraints
As of now, a simple power density model is used. GasTurb seems to suggest that the performances can be computed like that of an inverter. Would it be the same for mass ?
florentLutz
commented
1 year ago
As of now, a simple power density model is used. GasTurb seems to suggest that the performances can be computed like that of an inverter. Would it be the same for mass ?