Development of innovative and optimized stiffeners run-out for overall panel weight saving of composite wing
The objective here is to develop the tools and the methodology to optimize the design of a stiffener run-out on a composite stiffened panel (stiffener geometry, thicknesses and lay-ups of different components, shape of the tapering). Based on mechanical test of typical configurations, both simulations and failure criteria will be developed for strength predictions capability. This development shall lead to a simple methodology dedicated to support the design of innovative and improved panel configurations taking into account the plain area as well as the stiffener run-out. The validation of optimised solutions will be supported by mechanical tests. Please refer to the full and formal topic descriptions published in this call.
The objective of the Call is to develop digitalization of life cycle of Ground System Test based on Eco Design. These novel and advanced way to realise Ground Test, increases quality control and flexi...
An ECSEL Research and Innovation Action (RIA) primarily consists of activities aiming to establish new knowledge and/or to explore the feasibility of a new or improved technology, product, process, se...