Aeroelastic effects on the weight of an aircraft in the pre-design phase
Application of MDO to Large Subsonic Transport Aircraft
Wing primary structure weight estimation of transport aircrafts in the pre-development phase
Advanced Fuselage Weight Estimation for the New Generation of Transport Aircraft
Refined approaches for terrestrial reference frame computations
Investigation of local load introduction methods in aircraft pre-design
Influence of Aeroelastic Tailoring in the Multidisciplinary Design of a New Aircraft