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Opendata, web and dolomites

ASPIRE SIGNED

Aerodynamic and acouStic for high-by-Pass ratIo tuRbofan intEgration

Total Cost €

EC-Contrib. €

Partnership

Views

Outcomes and
results

ASPIRE project word cloud

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

lpa combination industrial performance aerodynamic acare nlr ogv coupling sria consistent ec efficiency tsagi manner configurations configuration coordinators air mobility wing 235 turbofan innovative cfp01 codes total uhbr tests integration motivated wind grant alignment leadership concerned 908 outside interactions efforts cs2 greening gathering validate cross request flight enhanced months itd purpose fan ultra 33 2014 acoustic dlr national ration designed iadp reference performed engine pass tunnel responds tremendous aircraft tools significantly ratio onera equipped transport close airframe engines individually pylon nacelle aspire jti numerical collaborative experimental understand core reliability partners 01 foreseen

Project "ASPIRE" 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	3˙406˙735 €
EC max contribution	2˙908˙234 € (85%)
Programme	1. H2020-EU.3.4.5.4. (ITD Airframe)
Code Call	H2020-CS2-CFP01-2014-01
Funding Scheme	CS2-RIA
Starting year	2016
Duration (year-month-day)	from 2016-01-01 to 2018-09-30

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES 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.	FR (PALAISEAU)	coordinator	1˙434˙531.00
2	DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV Organization address address: Linder Hoehe city: KOELN postcode: 51147 website: www.dlr.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 (KOELN)	participant	1˙009˙993.00
3	STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM 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.	NL (AMSTERDAM)	participant	463˙710.00
4	FEDERAL STATE UNITARY ENTERPRISE THE CENTRAL AEROHYDRODYNAMIC INSTITUTE NAMED AFTER PROF. N.E. ZHUKOVSKY FEDERAL STATE UNITARY ENTERPRISE THE CENTRAL AEROHYDRODYNAMIC INSTITUTE NAMED AFTER PROF. N.E. ZHUKOVSKY Organization address address: Zhukovsky str 1 city: ZHUKOVSKY postcode: 140180 website: www.tsagi.ru contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	RU (ZHUKOVSKY)	participant	0.00

Map

Project objective

The ASPIRE proposal, gathering DLR, NLR, ONERA and TsAGI, responds to the topic JTI-CS2-2014-CFP01-AIR-01-01 “Aerodynamic and acoustic capabilities developments for close coupling, high by-pass ration turbofan Aircraft integration”. The comprehensive experience of the partners working on innovative engine aircraft integration concepts both individually and in previous collaborative efforts motivated their common application. The high level objectives of the ASPIRE proposal lead to improve and validate numerical and experimental capabilities to assess the aerodynamic and acoustic performance of innovative aircraft configurations equipped with ultra-high by-pass ratio turbofan (UHBR). For that purpose, the numerical activities will be performed on a reference configuration partially designed by the consortium (generic fan/OGV combination) and by the lead industrial partner (nacelle, pylon, wing). Cross-comparison of codes are foreseen in specific tasks to improve the reliability of tools and better understand the tremendous interactions between airframe and UHBR engines. The experimental activities aim at improving the efficiency of acoustic means during wind-tunnel and flight tests. The ASPIRE total grant request to EC is 2 908 235 € for DLR, NLR and ONERA, the activities conducted by TsAGI being funded outside (national grant). The project will be conducted over 33 months in close alignment with the overall LPA-IADP and AIRFRAME-ITD needs and in agreement with the concerned IADP & ITD industrial coordinators and further selected and involved core partners and/or partners. The ASPIRE proposal will also be conducted in manner consistent with the other research activities performed in the AIRFRAME-ITD and the LPA-IADP. The integration of experimental and numerical capabilities will significantly contribute to ACARE SRIA 2, in terms of the greening of air transport, improving industrial leadership, and bringing enhanced mobility.

Publications

List of publications.
year	authors and title	journal	last update
2017	A. Holewa and S. GuÃ©rin Fan tone simulation from a UHBR engine with drooped nacelle inlet at Approach condition and an angle of attack of 10Â°. published pages: , ISSN: , DOI:	21st Workshop of the Aeroacoustics Specialists Committee of the CEAS, Dublin	2019-06-18
2018	C. Polacsek, A. Chelius, G. Billonnet, R. Barrier Tone noise prediction of a full-scale UHBR engine with/without inflow distorsion published pages: , ISSN: , DOI:	25th ICSV	2019-04-18
2019	R, Schnell, E. Goldhahn,M. Julian Design and performance of a Low Fan-Pressure-Ratio Propulsion System published pages: paper 24017, ISSN: , DOI:	ISABE-2019	2019-04-18

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