Numerical Method to Determine Structural Element Reduced Stiffness for Desired Composite Wing Structures Configurations
Autori:
Stammel, S.; Bisagni, C.
Pubblicato in:
34th Congress of the International Council of the Aeronautical Sciences (ICAS2024), 2024
Editore:
ICAS
Exploiting post-buckling nonlinearities for gust load reduction in high aspect ratio aircraft wings
Autori:
Farinha P., Toffol F. and Bisagni C.
Pubblicato in:
ECCOMAS conference proceedings, 2025
Editore:
ECCOMAS
Passive Method for Dynamic Loads Alleviation Using Structural Buckling in a Composite Wing
(si apre in una nuova finestra)
Autori:
Francesco Toffol, Chiara Bisagni
Pubblicato in:
AIAA SCITECH 2025 Forum, 2025
Editore:
American Institute of Aeronautics and Astronautics
DOI:
10.2514/6.2025-0425
Shape reconstruction of post-buckled panels in aWagner-Beam test-rig using distributed optical sensors and digital image correlation
Autori:
Aceti P., Stammel S., Sala G. and Bisagni C.
Pubblicato in:
15th International Workshop on Structural Health Monitoring, 2025
Editore:
15th International Workshop on Structural Health Monitoring
Gust Load Passive Alleviation by Means on Nonlinear, Buckling Driven, Structural Response
Autori:
Toffol, F.; Bisagni, C.
Pubblicato in:
34th Congress of the International Council of the Aeronautical Sciences (ICAS2024), 2024
Editore:
ICAS
NABUCCO Take-Off: Multi-Stable Panels for an Adaptive Wing
Autori:
Bisagni, C.
Pubblicato in:
34th Congress of the International Council of the Aeronautical Sciences (ICAS2024), 2024
Editore:
ICAS
