Zobrazeno 1 - 10
of 62
pro vyhledávání: '"Eelco Jansen"'
Efficient generation of geodesic random fields in finite elements with application to shell buckling
Publikováno v:
Thin-Walled Structures 179 (2022)
Structures contain inherent deviations from idealized geometry and material properties. Quantifying the effects of such random variations is of interest when determining the reliability and robustness of a structure. Generating fields that follow co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::986fbd7821281e85844a123d1cecb35a
https://www.repo.uni-hannover.de/handle/123456789/13662
https://www.repo.uni-hannover.de/handle/123456789/13662
Autor:
Sander van den Broek, Eelco Jansen, Alberto Pirrera, Paul M. Weaver, Raimund Rolfes, S. Minera
Publikováno v:
AIAA Journal. 58:2307-2320
The effect of stochastic variation in material and geometric properties on structural performance is important for robust design. Knowledge of such effects can be acquired by applying variation pat...
Autor:
Saullo G. P. Castro, Eelco Jansen
The multi-modal formulation of Koiter's asymptotic method provides a systematic and efficient procedure to evaluate the initial post-buckling behaviour and to assess the nonlinear behavior of structures. This manuscript presents a displacement-based
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::935a940c5f85a491087288e1de5bb909
https://engrxiv.org/92xvf
https://engrxiv.org/92xvf
Publikováno v:
Thin-Walled Structures. 139:219-231
A numerical study of damage behaviour in unidirectional Carbon Fibre Reinforced Plastics (CFRP) laminates at different stress ratios is self implemented. The study is conducted using the commercial finite element software ABAQUS employing a layer-bas
Publikováno v:
Mechanics of Advanced Materials and Structures. 26:48-55
Exploiting the anisotropic nature of composite laminates is a driving factor to improve the design regime of multistable structures. The concept of laminate tailoring is being taken a step ahead by allowing variation in fiber angle orientation within
This paper presents an analysis of a novel morphing trailing edge flap design for a wind turbine rotor blade with embedded multistable composite plates. Morphing trailing edge devices are promising candidates for reducing loads in variable wind condi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::29b14d7755e347a673d9355bafb9ce78
https://publica.fraunhofer.de/handle/publica/267105
https://publica.fraunhofer.de/handle/publica/267105
Publikováno v:
Haldar, A, Groh, R, Jansen, E, Weaver, P M & Rolfes, R 2020, ' An efficient semi-analytical framework to tailor snap-through loads in bistable variable stiffness laminates ', International Journal of Solids and Structures . https://doi.org/10.1016/j.ijsolstr.2020.02.018
Multistable laminates are potential candidates for adaptive structures due to the existence of multiple stable states. Commonly, such bistable shapes are generated from the cool-down process of the unsymmetric laminates from the curing temperature. I
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8c3bfa8a8b56e3577f9f25e9e4525f89
https://publica.fraunhofer.de/handle/publica/267100
https://publica.fraunhofer.de/handle/publica/267100
Publikováno v:
Thin-Walled Structures. 171:108735
Autor:
Raimund Rolfes, Felix Haase, Marc Köntges, Seyed Roozbeh Nabavi, Eelco Jansen, Jörg Käsewieter
Publikováno v:
IEEE Journal of Photovoltaics. 8:1510-1524
We experimentally analyze the position and opening behavior of cracks in multicrystalline silicon solar cells laminated in standard-sized frameless modules during mechanical loading in a 4-line-bending setup. The results of the experiment are reprodu
Publikováno v:
Composite Structures. 183:161-175
Multistable structures used in morphing applications are conventionally achieved by using unsymmetric laminates with straight fibers. An ideal morphing system always calls for a structure with highly anisotropic internal architecture. With the advanc