Possible advantages of a morphing solution replacing the traditional hinged movable aerodynamic surfaces will be analyzed in detail referring to different Aircraft configurations. Theoretical and numerical models will be developed in order to design the morphing structural configuration and to evaluate the performance of different torsional actuators systems. Finally an experimental prototype will be developed to asses and validate the concept.
Background and skills of ideal Doctoral Candidate:
Master in Aerospace Eng. with experience in aero-structural design and numerical simulation. Experience in aeroelastic design (numerical-experimental). Experience in structural optimization with commercial FEM codes (NASTRAN/LSDYNA other aeroelastic codes). Autonomy in solving complex problems. Ability to work in teams with different backgrounds. Ability to adapt to program variations.
Contacts: Prof. Enrico Cestino – enrico.cestino@polito.it; Prof. Giacomo Frulla – giacomo.frulla@polito.it.