Opendata, web and dolomites

ATTILA SIGNED

Advanced Testbed for TILtrotor Aeroelastics

Total Cost €

0

EC-Contrib. €

0

Partnership

0

Views

0

 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.

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

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).

Are you the coordinator (or a participant) of this project? Plaese send me more information about the "ATTILA" project.

For instance: the website url (it has not provided by EU-opendata yet), the logo, a more detailed description of the project (in plain text as a rtf file or a word file), some pictures (as picture files, not embedded into any word file), twitter account, linkedin page, etc.

Send me an  email (fabio@fabiodisconzi.com) and I put them in your project's page as son as possible.

Thanks. And then put a link of this page into your project's website.

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

More projects from the same programme (H2020-EU.3.4.5.3.)

RoCS (2019)

Rotorcraft Certification by Simulation

Read More  

STEADIEST (2019)

Design, development and flight qualification of a supercritical composite shaft drive line for tiltrotor main drive system

Read More  

SMAR-TeR (2019)

Next Generation of SMARt Active Inceptor for Tilt Rotor Application

Read More