MDO/MSO OF SLENDER THIN WALLED BOX BEAM MODEL (AIAA 2017-4323)
A Possible Adaptive Wing Apparatus for New UAV Configurations
Efficient Procedure for Robust Optimal Design of Aerospace Laminated Structures
Energy-absorbing origami structure for crashworthiness design
Aeroelastic Behaviour of Flexible Wings Carrying Distributed Electric Propulsion Systems