4   Artículos

 
en línea
Florent Grotto, Christophe Bouvet, Bruno Castanié and Joël Serra    
Aeronautical composite primary structures must evidence sufficient residual strength in the presence of damage for compliance with damage tolerance requirements. The study of stiffener debonding on panels subjected to compression after impact is performe... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Chang-Yull Lee, Jin-Young Jung and Se-Min Jeong    
Transient responses of stiffened panels with piezoelectric sensors and actuators are studied under normal blast loads. The air vehicles could be exposed to blast pulses generated by an explosion or shock-wave disturbances. Thus, active vibration suppress... ver más
Revista: Applied Sciences    Formato: Electrónico

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