Skip to main content
European Commission logo
TRIMIS

NEXT generation civil Tilt Rotor Interactional aerodynamic tail oPtimisation

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€2 777 223
EU Contribution
€2 582 757
Project Acronym
NEXTTRIP
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-CFP06-2017-01
Link to CORDIS
Objectives

The aerodynamic configuration definition of the NGCTR needs to be confirmed by a large-scale powered wind tunnel experiment, with the aim to verify and confirm the key choices of the configuration and to provide guidelines and proposals for potential additional improvement to be implemented. Within the EU 6th framework programme NICETRIP a 1/5th scale full-span, powered wind tunnel model has been designed and manufactured by NLR and tested in DNW-LLF and ONERA S1, with support of DLR.

In order to fully exploit the FP6 research program, NEXTTRIP is a 30 month- 2.77 MEuro valued project based on re-using the existing NICETRIP powered model and key-partners responsible for the successful execution of the NICETRIP low speed test.

The NEXTTRIP partners, NLR, DNW, DLR, Hit09 & Fokker will work together to modify the NICETRIP model, perform the wind tunnel test in DNW-LLF and define an optimal Empennage configuration based on the wind tunnel test results and given boundaries. NLR will coordinate the NEXTTRIP project and will perform wind tunnel model design and manufacture, test preparations (including GVT), advanced flow visualisation during wind tunnel test and wind tunnel data analysis. DNW will support test preparation and perform the wind tunnel test.

DLR will support test preparation and perform data-acquisition and piloting. Multi-objective aerodynamic empennage optimisation will be performed by Hit09 after wind tunnel data analysis. Fokker will, together with NLR, perform a verification of compliance with feasibility and industrial constraints during the empennage optimisation process.

For all three empennage configurations, both powered and unpowered test will be performed and for a selected configuration advance flow visualisation will be performed for a better understanding of the interactional aerodynamic phenomena.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.5.3.
Other Programme
JTI-CS2-2017-CFP06-FRC-01-15 Interactional aerodynamic assessment of advanced Tilt Rotor configuration

Partners

Lead Organisation
Organisation
Stichting Centrum Voor De Ontwikkeling Van Transport En Logistiek In Europa
Address
Van Nelleweg 1, 3044 BC Rotterdam, Netherlands
Organisation website
EU Contribution
€1 012 279
Partner Organisations
Organisation
Stichting Duits-Nederlandse Windtunnels
Address
VOORSTERWEG 31, 8316 PR Marknesse, Netherlands
Organisation website
EU Contribution
€1 101 972
Organisation
Deutsches Zentrum Fr Luft Und Raumfahrt E.v
Address
Linder Hoehe, 51147 KOELN, Germany
Organisation website
EU Contribution
€224 850
Organisation
Fokker Aerostructures Bv
Address
Industrieweg 4, 3351 LB Papendrecht, Netherlands
Organisation website
EU Contribution
€51 406
Organisation
Hit09 Srl
Address
Galleria Storione 8, 35100 Padova, Italy
EU Contribution
€192 250

Technologies

Technology Theme
Aircraft design and manufacturing
Technology
Heater layer for tilt rotorcraft
Development phase
Research/Invention

Contribute! Submit your project

Do you wish to submit a project or a programme? Head over to the Contribute page, login and follow the process!

Submit