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VENUS SIGNED

inVestigation of distributEd propulsion Noise and its mitigation through wind tUnnel experiments and numerical Simulations

Total Cost €

EC-Contrib. €

Partnership

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VENUS project word cloud

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

manufacturing integration cs2 aeroacoustic jti documents appropriate identification understand aerodynamic representative wind concurrent technologies benefits experimental propulsion electrical reduce venus cfp10 final tools practical experimentally emissions consist aeroacoustics standpoint aircraft advantage validation engines wing configurations tht distributed tested engine mitigation noise tunnel fuel installation theoretical achievement reference community deep wt tests models physics configuration optimized model article numerical electric framework pointed drastically landscape consumption regional 2018 dep performance 08 parametric realizing scientific data

Project "VENUS" data sheet

The following table provides information about the project.

Coordinator	UNIVERSITA DEGLI STUDI ROMA TRE Organization address address: VIA OSTIENSE 159 city: ROMA postcode: 154 website: www.uniroma3.it 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	Italy [IT]
Total cost	2˙282˙875 €
EC max contribution	2˙282˙875 € (100%)
Programme	1. H2020-EU.3.4.5.10. (Thematic Topics)
Code Call	H2020-CS2-CFP10-2019-01
Funding Scheme	CS2-RIA
Starting year	2020
Duration (year-month-day)	from 2020-04-01 to 2023-09-30

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	UNIVERSITA DEGLI STUDI ROMA TRE UNIVERSITA DEGLI STUDI ROMA TRE Organization address address: VIA OSTIENSE 159 city: ROMA postcode: 154 website: www.uniroma3.it contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IT (ROMA)	coordinator	750˙500.00
2	ELIGIO RE FRASCHINI SPA ELIGIO RE FRASCHINI SPA Organization address address: VIA XX SETTEMBRE 85 city: LEGNANO MILANO postcode: 20025 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IT (LEGNANO MILANO)	participant	422˙625.00
3	CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA Organization address address: Via Maiorise 1 city: CAPUA - CASERTA postcode: 81043 website: www.cira.it contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IT (CAPUA - CASERTA)	participant	378˙500.00
4	NHOE - SOCIETA' A RESPONSABILITA' LIMITATA NHOE - SOCIETA' A RESPONSABILITA' LIMITATA Organization address address: VIA SANGRO 5 city: POMEZIA postcode: 40 website: www.nhoe.it contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IT (POMEZIA)	participant	375˙000.00
5	IBK-INNOVATION GMBH & CO. KG IBK-INNOVATION GMBH & CO. KG Organization address address: BUTENDEICHSWEG 2 city: HAMBURG postcode: 21129 website: www.ibk-innovation.de contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (HAMBURG)	participant	356˙250.00

Map

Project objective

Distributed Electric Propulsion (DEP), is one of the propulsion configurations that, taking advantage from the Distributed Propulsion concept, is believed to exploit the benefits of electrical engines to drastically reduce fuel consumption and emissions. In the framework of the topic JTI-CS2-2018-CFP10-THT-08, the proposal VENUS will have the objective to understand the physics behind the aeroacoustics of DEP through a deep theoretical, experimental and numerical study. Appropriate numerical procedures for DEP noise assessment will be set-up and experimental data-set obtained in dedicated wind tunnel tests, will be used both as experimental DEP noise validation reference and for providing support to the identification of the main parameters affecting DEP noise. Technologies for DEP noise reduction will be studied as well and tested experimentally. From the technical standpoint, the VENUS consortium will support the model design, manufacturing and integration by realizing a representative test article for WT parametric aeroacoustic tests, able to allow for configuration changes, in terms of engine-wing and engine-engine installation configurations, and to test the selected noise mitigation technologies. The consortium will develop methods and tools enabling a concurrent aerodynamic and aeroacoustic design of DEP configuration aircraft. The final step will consist in the experimental-numerical assessment of the numerical models. As a practical achievement, the study will support the design of a new regional aircraft configuration, in terms of wing and engines’ installation, to target a DEP which is optimized in terms of aerodynamic and aeroacoustic performance. It is pointed out that all the produced models, data and documents will be open access for other institutions, with the objective to establish an “open test-case” for the whole European scientific community, unique in the aircraft design landscape.

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