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ATTILA SIGNED

Advanced Testbed for TILtrotor Aeroelastics

Total Cost €

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EC-Contrib. €

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Partnership

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 ATTILA project word cloud

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

54    tdt    flutter    56    261    capability    fidelity    proprotor    aeroelastically    instrumented    profit    simulations    introduction    froude    action    subcontractor    sensor    damping    centres    complementary    rotating    stiffness    speed    demonstration    tunnel    suitably    wind    safety    dynamic    2025    worldwide    aircraft    half    nasa    highest    6x6m    manufacture    codes    scaling    subjected    nacelle    verified    3x25    llf    code    contactless    provides    polimi    td    2024    months    dlr    aeroelastic    consist    nlr    power    flight    gathering    mass    section    coupled    shakedown    ensured    first    transonic    attila    dynamics    experimental    time    prior    525    correlation    full    cantilevered    testbed    fiber    foundation    size    model    post    scaled    analytical    productivity    validated    gas    technobis    least    sme    speeds    iterations    valued    university    structural    configurations    mach    representative    tiltrotor    wing    techniques    whirl    transfer    simultaneous    campaign    heavy    points    powered    models    performed    data    modal    engaging    dnw    meeting    optic    ngctr   

Project "ATTILA" data sheet

The following table provides information about the project.

Coordinator
STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM 

Organization address
address: Anthony Fokkerweg 2
city: AMSTERDAM
postcode: 1059CM
website: www.nlr.nl

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 Netherlands [NL]
 Total cost 5˙614˙013 €
 EC max contribution 5˙614˙013 € (100%)
 Programme 1. H2020-EU.3.4.5.3. (IADP Fast Rotorcraft)
 Code Call H2020-CS2-CFP09-2018-02
 Funding Scheme CS2-RIA
 Starting year 2019
 Duration (year-month-day) from 2019-11-01   to  2023-12-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM NL (AMSTERDAM) coordinator 3˙752˙812.00
2    DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV DE (KOELN) participant 1˙132˙751.00
3    STICHTING DUITS-NEDERLANDSE WINDTUNNELS NL (Marknesse) participant 381˙950.00
4    POLITECNICO DI MILANO IT (MILANO) participant 180˙000.00
5    TECHNOBIS FIBRE TECHNOLOGIES BV NL (ALKMAAR) participant 166˙500.00

Map

 Project objective

The ATTILA project is aimed at the design, manufacture and testing of an advanced testbed for aeroelastic wind tunnel testing of tiltrotor aircraft. The testbed will consist of a suitably instrumented aeroelastically scaled cantilevered half-wing with powered nacelle-proprotor system representative of the full-scale NGCTR-TD design. Advanced fiber optic sensor and contactless rotating power and data transfer techniques will be used. The design process, coupled with test iterations, is supported by detailed structural and aeroelastic simulations using a range of complementary codes. The ATTILA testbed will first be subjected to a wind-on shakedown test in the DNW LLF 6x6m test section in Froude scaled conditions. After the system functionality and structural dynamic characteristics have been verified, a second data gathering test will be performed in the NASA TDT heavy-gas transonic dynamics wind tunnel in simultaneous Froude and Mach scaled conditions, selected as subcontractor to NLR for its unique worldwide capability of meeting the full test requirements in terms of aeroelastic scaling capability, test Mach number, and model size. Testing will be performed in three mass/stiffness configurations covering 3x25 test points with test speeds up to the NGCTR-TD whirl flutter speed (at least M = 0.56). The proposed test campaign provides the highest possible fidelity experimental demonstration of the whirl flutter characteristics of the NGCTR-TD prior to high-speed flight testing in 2024-2025. Its productivity and safety will be ensured through the introduction of real-time modal damping analysis. The post-test data analysis phase includes a test-to-code correlation study in which the analytical models derived by the consortium are validated against the test results. Engaging a significant subcontractor (NASA), this 54-months €6,525,261 valued action is composed of 2 research centres (NLR, DLR), 1 non-profit foundation (DNW), 1 university (POLIMI) and 1 SME (Technobis).

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

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