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CA3ViAR SIGNED

Composite fan Aerodynamic, Aeroelastic, and Aeroacoustic VAlidation Rig

Total Cost €

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EC-Contrib. €

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Partnership

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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 DE (HAMBURG) coordinator 792˙500.00
2    TECHNISCHE UNIVERSITAET BRAUNSCHWEIG DE (BRAUNSCHWEIG) participant 944˙000.00
3    GOTTFRIED WILHELM LEIBNIZ UNIVERSITAET HANNOVER DE (HANNOVER) participant 468˙750.00
4    DREAM INNOVATION SRL 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.

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