A study of the dynamic effects on the design loads of a civil aircraft
M Bronstein
E Feldman
R Vescovini
Chiara Bisagni (Politecnico di Milano, TU Delft - Aerospace Structures & Computational Mechanics)
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Abstract
The daedalos project was supported by the european commission under the programme transport (including aeronautics) of the 7th framework programme for research and technological development, grant agreement no: 266411. Daedalos stands for dynamics in aircraft engineering design and analysis for light optimized structures The primary objective of the daedalos project is to investigate the dynamic effects on the actual loads acting on the airframe for improved definition of the sizing loads for structural components of civil aircrafts.