Numerical Method to Determine Structural Element Reduced Stiffness for Desired Composite Wing Structures Configurations
Autoren:
Stammel, S.; Bisagni, C.
Veröffentlicht in:
34th Congress of the International Council of the Aeronautical Sciences (ICAS2024), 2024
Herausgeber:
ICAS
Exploiting post-buckling nonlinearities for gust load reduction in high aspect ratio aircraft wings
Autoren:
Farinha P., Toffol F. and Bisagni C.
Veröffentlicht in:
ECCOMAS conference proceedings, 2025
Herausgeber:
ECCOMAS
Passive Method for Dynamic Loads Alleviation Using Structural Buckling in a Composite Wing
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Autoren:
Francesco Toffol, Chiara Bisagni
Veröffentlicht in:
AIAA SCITECH 2025 Forum, 2025
Herausgeber:
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
Autoren:
Aceti P., Stammel S., Sala G. and Bisagni C.
Veröffentlicht in:
15th International Workshop on Structural Health Monitoring, 2025
Herausgeber:
15th International Workshop on Structural Health Monitoring
Gust Load Passive Alleviation by Means on Nonlinear, Buckling Driven, Structural Response
Autoren:
Toffol, F.; Bisagni, C.
Veröffentlicht in:
34th Congress of the International Council of the Aeronautical Sciences (ICAS2024), 2024
Herausgeber:
ICAS
NABUCCO Take-Off: Multi-Stable Panels for an Adaptive Wing
Autoren:
Bisagni, C.
Veröffentlicht in:
34th Congress of the International Council of the Aeronautical Sciences (ICAS2024), 2024
Herausgeber:
ICAS
