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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.

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

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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