Print Email Facebook Twitter A study of the dynamic effects on the design loads of a civil aircraft Title A study of the dynamic effects on the design loads of a civil aircraft Author Bronstein, M Feldman, E Vescovini, R Bisagni, C. (TU Delft Aerospace Structures & Computational Mechanics; Politecnico di Milano) Date 2016 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. To reference this document use: http://resolver.tudelft.nl/uuid:41ff1c90-3b78-412c-9fda-b97613bcea81 Source Proceedings of 56th Israel Annual Conference on Aerospace Sciences: Tel-Aviv & Haifa, Israel Event 56th Israel Annual Conference on Aerospace Sciences, 2016-03-09 → 2016-03-10, Tel-Aviv & Haifa, Israel Part of collection Institutional Repository Document type conference paper Rights © 2016 M Bronstein, E Feldman, R Vescovini, C. Bisagni Files PDF 2016_Bisagni_Conf_IACAS.pdf 978.21 KB Close viewer /islandora/object/uuid:41ff1c90-3b78-412c-9fda-b97613bcea81/datastream/OBJ/view