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Powered, modular Wind-Tunnel model for low and high Reynolds tests

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€3 932 576
EU Contribution
€2 841 943
Project website
Project Acronym
POLITE
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Environmental/Emissions aspects
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP02-2015-01
Link to CORDIS
Objectives

POLITE answers the CfP JTI-CS2-2015-CFP02-REG-02-02, published in the second batch of the JTI-Cleansky 2. Within the work-package linked to CS2 a so-called flying test bed (FTB) is developed and used for analyzing and validating technologies developed within CS2, domain REG. This is clearly in line with Cleansky 2, which includes, among other topics, to deliver innovative technologies that are validated in relevant conditions (in this case flight test). Before such a complex test can be performed a high level of confidence in the technologies developed is necessary. POLITE answers this need, since it enables low and high Reynolds WT-tests that allow to validating technologies to improve performances in low and high speed. Increasing the aircraft performance is supporting not only the CS2-workplan but also the ACARE2020 vision by allowing passengers to travel with reduced fuel burn and there increasing the ecologic efficiency of the aircraft.

Within POLITE a consortium build from 4 different partners will tackle all relevant topics. The consortium is build up in way that all necessary domains are covered. In particular, three partners the consortium includes

  • ARA with a strong competence in model design activities and manufacturing
  • IBK with a good experience in developing large, specialised models
  • DREAM with a very good expertise in aerodynamics and model design in particular
  • RUAG involving the background on powered models and introducing the technology necessary for the engines. Their LWTE is the solution candidate for the low-Re tests.

Additionally, to this ONERA will be included via subcontracting. ONERA has a strong background in air-driven motors which are used in the pressurized WT ONERA F1. They will introduce this technology into the consortium for implementation into the model used for high-Re tests.

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
Ibk Ingenieurbuero Dr Kretzschmar
Address
Rehdorfer Str. 4, 90431 NUREMBERG, Germany
Organisation website
EU Contribution
€332 500
Partner Organisations
Organisation
Dream Innovation Srl
Address
VIA F. PARRI 1, 81030 SANT'ARPINO, Italy
EU Contribution
€572 000
Organisation
Dream Innovation Srl
Address
VIA F. PARRI 1, 81030 SANT'ARPINO, Italy
EU Contribution
€144 375
Organisation
Aircraft Research Association Limited
Address
Manton Lane, Bedford, MK41 7PF, United Kingdom
Organisation website
EU Contribution
€1 110 119
Organisation
Aircraft Research Association Limited
Address
Manton Lane, Bedford, MK41 7PF, United Kingdom
Organisation website
EU Contribution
€2 365 068
Organisation
Ruag Aerospace
Address
Seetalstrasse 175, 175 EMMEN, Switzerland
Organisation website
EU Contribution
€50 000
Organisation
Ruag Aerospace
Address
Seetalstrasse 175, 175 EMMEN, Switzerland
Organisation website
EU Contribution
€0

Technologies

Technology Theme
Aircraft design and manufacturing
Technology
Aircraft design model
Development phase
Research/Invention

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