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Opendata, web and dolomites

CA3ViAR SIGNED

Composite fan Aerodynamic, Aeroelastic, and Aeroacoustic VAlidation Rig

Total Cost €

EC-Contrib. €

Partnership

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CA3ViAR project word cloud

Explore the words cloud of the CA3ViAR project. It provides you a very rough idea of what is the project "CA3ViAR" about.

instability responsible tests luh civil ltf measuring mungsmachinen ouml flutter literature italian conceived acoustic stall universit models uhbr validation article manufacturing hannover aerodynamic shaping auml review manufacturer germany experimental aeroelasticity blades uuml led ca3viar instabilities institut braunschweig perform ibk wt geometry facility aeroacoustics mechanically materials propulsion fan technische tunnel ptf subcontracting sme engine composite aero performance transonic representative acquired rotor metallic flugantriebe wind operations aircrafts aeroelastic str initially tub supervision ifas leibniz eventual made und performed mechanisms parts dream data last instrumentation calibration designed fans specialized integration investigation

Project "CA3ViAR" data sheet

The following table provides information about the project.

Coordinator	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.
Coordinator Country	Germany [DE]
Total cost	2˙296˙875 €
EC max contribution	2˙296˙875 € (100%)
Programme	1. H2020-EU.3.4.5.10. (Thematic Topics)
Code Call	H2020-CS2-CFP09-2018-02
Funding Scheme	CS2-RIA
Starting year	2019
Duration (year-month-day)	from 2019-09-01 to 2023-08-31

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	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)	coordinator	792˙500.00
2	TECHNISCHE UNIVERSITAET BRAUNSCHWEIG TECHNISCHE UNIVERSITAET BRAUNSCHWEIG Organization address address: UNIVERSITAETSPLATZ 2 city: BRAUNSCHWEIG postcode: 38106 website: www.tu-braunschweig.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 (BRAUNSCHWEIG)	participant	944˙000.00
3	GOTTFRIED WILHELM LEIBNIZ UNIVERSITAET HANNOVER GOTTFRIED WILHELM LEIBNIZ UNIVERSITAET HANNOVER Organization address address: Welfengarten 1 city: HANNOVER postcode: 30167 website: www.uni-hannover.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 (HANNOVER)	participant	468˙750.00
4	DREAM INNOVATION SRL DREAM INNOVATION SRL Organization address address: VIA F. PARRI 1 city: SANT'ARPINO postcode: 81030 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 (SANT'ARPINO)	participant	91˙625.00

Map

Project objective

The main aim of the CA3ViAR project is the design of an Open-Test-Case Fan geometry that will develop instability mechanisms which are representative for UHBR fans of civil aircrafts and perform a comprehensive experimental investigation to measure aerodynamic, aeroelastic and aero-acoustic performance in a wide range of operational conditions. Experimental tests will be performed in the Propulsion-Test-Facility (PTF) of the Institut für Flugantriebe und Strömungsmachinen (IFAS) of Braunschweig, Germany. The proposal CA3ViAR will target several objectives. Initially a literature review of the main issues affecting composite UHBR engine fans will be performed by the Technische Universität Braunschweig (TUB). The design of the Low-Transonic Fan (LTF) will be led by TUB with support from DREAM (an Italian SME) in terms of aerodynamic shaping as well as from Leibniz Universität Hannover (LUH) and IBK in terms of aeroelasticity and aeroacoustics. The LTF test article, to be mechanically designed by IBK, will be conceived in a way to experience aerodynamic and aeroelastic instabilities in an expected way during wind-tunnel operations. Manufacturing-related activities will be performed under IBK supervision through subcontracting to well-recognized manufacturer specialized in rotor blades and parts made of composite and metallic materials, while requirements for the test article integration will be provided by TUB, responsible of WT instrumentation and operations. The execution of the experimental tests aimed at measuring fan instabilities (e.g. stall, flutter, etc.) will be performed by TUB with support from LUH. The last technical phase of the project will be the calibration and the eventual validation of aerodynamic, aeroelastic and aero-acoustic models according to WT test data acquired in the PTF. This last technical phase will be led by LUH, with a strong support from all the other partners.

Deliverables

List of deliverables.
Plan for the Exploitation and Dissemination of Results	Documents, reports	2020-03-09 16:04:55
Data Management Plan	Open Research Data Pilot	2020-03-06 13:50:52
Literature review and LTF aero design requirements	Documents, reports	2020-02-12 12:17:58

Take a look to the deliverables list in detail: detailed list of CA3ViAR deliverables.

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The information about "CA3VIAR" are provided by the European Opendata Portal: CORDIS opendata.