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DOVER SIGNED

Methodology Development and Validation of WEight Optimized Stiffeners Run-Out Design for Future Composite Wings

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

DOVER project word cloud

Explore the words cloud of the DOVER project. It provides you a very rough idea of what is the project "DOVER" about.

designing generate weight initial structured numerical stages panel 32 reliability lay fasteners correlated span damage model outs stiffener stage validated base tapering accuracy strain optimized innovative investigation geometries manufactured thicknesses configurations quality run predict economical shape fatigue methodology savings wing experimental structural designer tool stress life solutions environment tolerance configuration global carry solution dover stacking composite final maximum validate sequences panels campaigns considerable obtain models capability criteria components put peeling create ups time expensive anti tests ing lightweight mono shapes geometry prediction optimization

Project "DOVER" data sheet

The following table provides information about the project.

Coordinator	UNIVERSIDAD DE SEVILLA Organization address address: CALLE S. FERNANDO 4 city: SEVILLA postcode: 41004 website: www.us.es contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.
Coordinator Country	Spain [ES]
Project website	http://www.dover-project.eu
Total cost	742˙430 €
EC max contribution	742˙430 € (100%)
Programme	1. H2020-EU.3.4.5.4. (ITD Airframe)
Code Call	H2020-CS2-CFP06-2017-01
Funding Scheme	CS2-RIA
Starting year	2018
Duration (year-month-day)	from 2018-03-01 to 2020-10-31

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	UNIVERSIDAD DE SEVILLA UNIVERSIDAD DE SEVILLA Organization address address: CALLE S. FERNANDO 4 city: SEVILLA postcode: 41004 website: www.us.es contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	ES (SEVILLA)	coordinator	387˙951.00
2	SOFITEC AERO SL SOFITEC AERO SL Organization address address: AUTOV A-4 KM 521 PARQUE LOGISTICO E INDUSTRIAL MAN LB NAVE 1 city: CARMONA postcode: 41410 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	ES (CARMONA)	participant	230˙500.00
3	PACHECO RAMOS GUILLERMO PACHECO RAMOS GUILLERMO Organization address address: CALLE HUELVA 10 city: TOMARES postcode: 41940 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	ES (TOMARES)	participant	123˙978.00

Map

Project objective

DOVER aims to develop a design optimization tool and methodology dedicated to support the design of innovative and weight-optimized composite panel configurations with capability to improve all areas and configuration parameters such as geometries, stacking sequences or anti-peeling fasteners. The resulting methodology accuracy and reliability is to be validated by means of experimental tests. The project will be carried out in a 32-month time span. DOVER solution proposal is to create and validate a design tool and methodology that enables optimization of wing structural composite panels. The developed tool will provide an environment for the investigation of innovative lightweight shapes including stiffener geometry, thicknesses and lay-ups of different components, shape of the tapering or anti-peeling fasteners configuration. By means of this tool, the designer will be able to predict the failure of any stiffener run-out configuration and obtain a global panel optimization with considerable time savings, because it will not require any complex numerical models to predict behaviour, and economical, because it will not be necessary to carry out expensive testing campaigns. To achieve this solution, DOVER is structured in different stages that ensure maximum quality, accuracy and reliability. An initial experimental study of stiffener run-out behaviour will establish an experimental base that will be used to develop a model and to generate failure criteria prediction methodology. This methodology will be put in practice by designing different configurations of innovative stiffener run-outs. Optimized solutions will be evaluated and correlated against experimental results. For that, at a final stage, mono and multi stiffener panels will be manufactured, and stress and strain, damage tolerance and fatigue life will be obtained through experimental testing to validate the development.

Deliverables

List of deliverables.
D5.2 Dissemination and exploitation plan	Documents, reports	2019-04-05 17:12:17
D5.1 Data management Plan	Open Research Data Pilot	2019-04-09 16:27:17
D1.1 - Test definition programme	Documents, reports	2019-04-09 16:27:13

Take a look to the deliverables list in detail: detailed list of DOVER deliverables.

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The information about "DOVER" are provided by the European Opendata Portal: CORDIS opendata.