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Dynamics in Aircraft Engineering Design and Analysis for Light Optimized Structures (DAEDALOS)
Date du début: 1 nov. 2010, Date de fin: 30 avr. 2014,
"Today’s design and certification procedures of aircrafts are mainly based on conservative static loading which leads to additional weight and, potentially, to a structurally unsafe aircraft. The overall objective of the DAEDALOS project is to develop methods and procedures to determine dynamical loads considering the effects of dynamic buckling, material damping and mechanical hysteresis during a ...
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