A study of the dynamic effects on the design loads of a civil aircraft

Conference paper (2016)

Authors

C. Bisagni Politecnico di Milano, Aerospace Structures & Computational Mechanics - Aerospace Engineering
Research Group
Aerospace Structures & Computational Mechanics (Aerospace Engineering) (TU Delft)
Copyright: © 2016 M Bronstein, E Feldman, R Vescovini, C. Bisagni
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Published Date

2016

Language

English

Reuse Rights

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Aerospace Structures & Computational Mechanics

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.