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INAFLOWT SIGNED

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

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

INAFLOWT project word cloud

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

tunnel benefits goals afc active moving arrays pave wing prove aflonext inaflowt suction combinations innovative actuator engine tested geometry commercial generate vast uhbr bypass cfd record model reynolds simulations boundary pylon engines extensive aerodynamic guarantee successful near environment blowing simplified wind layer reliability collaborations combined lift saob prototypes aviation ratio outputs realistic small configuration separation experts industrial consist representative flow bench parts progress oscillatory efficiency steady ultra realization excellence aircraft combination numerical

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 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.	IL (TEL AVIV)	coordinator	360˙000.00
2	UNIVERSITAET STUTTGART UNIVERSITAET STUTTGART Organization address address: KEPLERSTRASSE 7 city: STUTTGART postcode: 70174 website: www.uni-stuttgart.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 (STUTTGART)	participant	130˙000.00
3	VYZKUMNY A ZKUSEBNI LETECKY USTAV AS VYZKUMNY A ZKUSEBNI LETECKY USTAV AS Organization address address: LETNANY BERANOVYCH 130 city: PRAHA 18 postcode: 19000 website: www.vzlu.cz contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	CZ (PRAHA 18)	participant	130˙000.00
4	ISRAEL AEROSPACE INDUSTRIES LTD. ISRAEL AEROSPACE INDUSTRIES LTD. Organization address address: BEN GURION INTERNATIONAL AIRPORT city: LOD postcode: 70100 website: www.iai.co.il contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IL (LOD)	participant	80˙000.00
5	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 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

List of publications.
year	authors and title	journal	last update
2019	Junaid Ullah, Ales PrachaÅ™, Miroslav Å mÃd, Avraham Seifert, Vitaly Soudakov, Thorsten Lutz, Ewald KraÌˆmer 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 KraÌˆmer 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.; PrachaÅ™, A.; HospodÃ¡Å™, 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, AleÅ¡ PrachaÅ™, Pavel HospodÃ¡Å™ 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.