Opendata, web and dolomites

CONCERTO SIGNED

Computation of cOmpouNd rotorCraft latEral RoTor nOise

Total Cost €

0

EC-Contrib. €

0

Partnership

0

Views

0

Project "CONCERTO" data sheet

The following table provides information about the project.

Coordinator
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES 

Organization address
address: CHEMIN DE LA HUNIERE
city: PALAISEAU
postcode: 91120
website: www.onera.fr

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 France [FR]
 Total cost 634˙936 €
 EC max contribution 634˙936 € (100%)
 Programme 1. H2020-EU.3.4.5.3. (IADP Fast Rotorcraft)
 Code Call H2020-CS2-CFP06-2017-01
 Funding Scheme CS2-RIA
 Starting year 2018
 Duration (year-month-day) from 2018-03-01   to  2021-02-28

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES FR (PALAISEAU) coordinator 382˙192.00
2    DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV DE (KOELN) participant 252˙743.00

Map

 Project objective

The main objective of the CONCERTO project is to provide the topic leader (Airbus Helicopters) of the Clean Sky 2 IADP Fast Rotorcraft with a new computational tool enabling the noise modelling and prediction of lateral rotors installed on the future LifeRCraft demonstrator. This tool, enabling both fast prediction and high fidelity approaches, will include 3 modules: aerodynamics, free field acoustic and scattering effects. All three will be, implemented in a chaining process, based on a seamless workflow and software environment that will be created during the project. While aerodynamics module relies on PUMA code (Free Wake) as Fast aerodynamic solver and TAU code (CFD) as High fidelity solver, free field acoustic solver will use the KIM code (FW-H). KIM code will also be implemented for fast scattered acoustic prediction, while BEMUSE code (BEM) will be implemented for high fidelity scattered prediction. The overall tool will be validated and applied to a subset of the LifeRCraft flight domain. The project will be implemented through 6 WPs: WP1 Workflow definition and implementation; WP2 Aerodynamics module; WP3 Free-field acoustic module; WP4 Scattered field acoustic module; WP5 Validation; WP6 Project Management, dissemination and exploitation. CONCERTO consortium, ONERA and DLR, will deliver and install the necessary tools at the topic leader location including documentation, support and possible updates during the 3 years of the project. With a total budget of about € 635,000, the project will go beyond the state of the art (investigating unsteady flight cases, capturing quadripole noise sources, solving efficiently the multi-frequency problem of combined main rotor and lateral rotors, etc.), and will fully address user needs, contribute to the maturation and future commercialization of a new aircraft vehicle satisfying new mobility roles, thus contributing to the competitiveness of the European aeronautics sector.

 Deliverables

List of deliverables.
Plan for the Exploitation and Dissemination of the project results Documents, reports 2019-10-29 14:24:51

Take a look to the deliverables list in detail:  detailed list of CONCERTO deliverables.

Are you the coordinator (or a participant) of this project? Plaese send me more information about the "CONCERTO" 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 "CONCERTO" are provided by the European Opendata Portal: CORDIS opendata.

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

SMAR-TeR (2019)

Next Generation of SMARt Active Inceptor for Tilt Rotor Application

Read More  

TRIcEPS (2019)

Tilt Rotor Integrated Air Intake and Engine Protection Systems

Read More  

RoCS (2019)

Rotorcraft Certification by Simulation

Read More