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TRIMIS

Large scale wind tunnel turboprop aircraft model integrating morphing devices for aerodynamic experimental assessment

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€1 534 250
EU Contribution
€1 295 875
Project Acronym
WTM-RECYCLE
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Other specified
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP04-2016-02
Link to CORDIS
Objectives

WTM-RECYCLE addresses the call JTI-CS2-2016-CFP04-REG-01-05 and will in total re-design an existing WT-model (designed and manufacturing in the JTI-CS-project LOSITA), manufacture the new parts and implement them in into the model and finally perform a WT-tests focused on delivering aerodynamic data. The results will be post-processed and implemented into an aerodynamic database supported by CFD.

The model updates to be performed focus on changes that can be roughly summarized in two groups:

a.) At first model updates reflecting a new design state are implemented (e.g. fuselage geometry, fuselage length).

b.) Solutions developed within the REG-ITD which shall be tested and assessed in the WT. This specifically involves the morphing LE, TE and winglet, which shall be used as High-Lift devices.

The project addressing this task is organized straight-forward using a consortium of three partners that have proven their competence in WT-model design, aerodynamic analysis and assessment as well as manufacturing in recent R&D projects. WT-test activities are subcontracted to the RUAG-WT, which is the obvious choice for test including this model. In total, the project strongly benefits from the experience with the initial model of two of the partners (IBK and EUROTECH) obtained in the LOSITA-project, since they will also support the WTM-RECYCLE project.

Finally, an aerodynamic assessment and an extrapolation towards full-scale will be performed under the responsibility of KTH in order to display the benefits of the new High-Lift-devices.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.5.2.

Partners

Lead Organisation
Organisation
Kungliga Tekniska Hoegskolan
Address
Brinellvagen 8, 100 44 Stockholm, Sweden
EU Contribution
€745 500
Partner Organisations
Organisation
Ibk Ingenieurbuero Dr Kretzschmar
Address
Rehdorfer Str. 4, 90431 NUREMBERG, Germany
Organisation website
EU Contribution
€248 500
Organisation
Eurotech Di Mario Amoroso Sas
Address
Via Luigi Mercantini 23 IS 8, 80125 NAPOLI, Italy
Organisation website
EU Contribution
€301 875

Technologies

Technology Theme
Aircraft design and manufacturing
Technology
Morphing wing
Development phase
Research/Invention

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