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INAFLOWT SIGNED

INnovative Actuation Concepts for Engine/Pylon/Wing Separation FLOw Control (Design, Build and Wind Tunnel Test)

Total Cost €

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EC-Contrib. €

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Partnership

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Project "INAFLOWT" data sheet

The following table provides information about the project.

Coordinator
TEL AVIV UNIVERSITY 

Organization address
address: RAMAT AVIV
city: TEL AVIV
postcode: 69978
website: http://www.tau.ac.il/

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 Israel [IL]
 Project website http://web.eng.tau.ac.il/
 Total cost 1˙146˙750 €
 EC max contribution 700˙000 € (61%)
 Programme 1. H2020-EU.3.4.5.1. (IADP Large Passenger Aircraft)
 Code Call H2020-CS2-CFP04-2016-02
 Funding Scheme CS2-RIA
 Starting year 2017
 Duration (year-month-day) from 2017-06-01   to  2020-09-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    TEL AVIV UNIVERSITY IL (TEL AVIV) coordinator 360˙000.00
2    UNIVERSITAET STUTTGART DE (STUTTGART) participant 130˙000.00
3    VYZKUMNY A ZKUSEBNI LETECKY USTAV AS CZ (PRAHA 18) participant 130˙000.00
4    ISRAEL AEROSPACE INDUSTRIES LTD. IL (LOD) participant 80˙000.00
5    FEDERAL STATE UNITARY ENTERPRISE THE CENTRAL AEROHYDRODYNAMIC INSTITUTE NAMED AFTER PROF. N.E. ZHUKOVSKY RU (ZHUKOVSKY) participant 0.00

Map

 Project objective

The objective of the INAFLOWT project is to use combinations of existing active flow control (AFC) concepts to generate a major advance in AFC aerodynamic efficiency and reliability. Steady suction in combination with oscillatory blowing will be combined using arrays of the no-moving parts SaOB actuator. Active boundary layer separation control concepts will be studied using numerical simulations, as well as with bench-top, simplified geometry and small scale wind tunnel testing. The most promising concept will be tested, integrated as real-scale prototypes in a large wind tunnel model representative of the ultra-high bypass ratio (UHBR) engine/pylon/wing/high-lift system configuration, already tested within AFLONEXT, at realistic Reynolds number, to prove results in near industrial environment. The INAFLOWT consortium consist of known experts with vast experience and extensive excellence record of collaborations in the areas of AFC, high-lift aerodynamic, wind tunnel testing and CFD simulations. These capabilities and features will guarantee the successful realization of the ambitious goals of the INAFLOWT project and will progress the proposed AFC configuration beyond the State-of-the-Art. The outputs are ambitious and innovative and will pave the way to operational use of UHBR engines in commercial aircraft which will provide significant operational benefits of future European aviation products.

 Deliverables

List of deliverables.
Plan for Dissemination and Exploitation of Results (PDER) Documents, reports 2020-02-12 11:11:22

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

 Publications

year authors and title journal last update
List of publications.
2019 Junaid Ullah, Ales Prachař, Miroslav Šmíd, Avraham Seifert, Vitaly Soudakov, Thorsten Lutz, Ewald Krämer
Reynolds Number and Wind Tunnel Wall Effects on the Flow Field on a Generic UHBR Engine High-Lift Configuration
published pages: , ISSN: , DOI:
Conference: 54th 3AF International 2020-02-12
2019 M. Possti, A. Yaniv, J. Ullah and A. Seifert (Tel-Aviv University/IAG Stuttgart)
Active control of wing-engine-slat cut-out region flow separation
published pages: , ISSN: , DOI:
Conference: 54th 3AF International 2020-02-12
2018 Junaid Ullah, Nimrod Shay, Maayan Possti, Avraham Seifert, Thorsten Lutz, Ewald Krämer
Capability of RANS Simulations to Reproduce Flat Plate Boundary Layer Interaction with Suction and Oscillatory Blowing
published pages: , ISSN: , DOI:
Conference: 21.STAB-Symposium 2020-02-12
2017 Vrchota, P.; Prachař, A.; Hospodář, P.; Dolgopyat, D.; Seifert, A.
Development and Verification of Simplified Boundary Condition of SaOB Actuator
published pages: , ISSN: , DOI:
March 2018: 58th Israel Annual Conference on Aerospace Sciences, 2020-02-12
2019 Petr Vrchota, Aleš Prachař, Pavel Hospodář
Verification of Boundary Conditions Applied to Active Flow Circulation Control
published pages: 34, ISSN: 2226-4310, DOI: 10.3390/aerospace6030034
Aerospace 6/3 2020-02-12

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

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