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

Informations projet

INAFLOWT

N° de convention de subvention: 754307

DOI

10.3030/754307

Projet clôturé

Date de signature de la CE 22 Mai 2017

Date de début 1 Juin 2017

Date de fin 30 Septembre 2020

Financé au titre de

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Coût total

€ 1 146 750,00

Contribution de l’UE

€ 700 000,00

Coordonné par

TEL AVIV UNIVERSITY
Israel

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Les liens vers les livrables et les publications des projets du 7e PC, ainsi que les liens vers certains types de résultats spécifiques tels que les jeux de données et les logiciels, sont récupérés dynamiquement sur OpenAIRE .

Livrables

Documents, reports (1)

Plan for Dissemination and Exploitation of Results (PDER)

Provide a plan (incl. dates, venues and targeted audience) to the project participants in order to implement a common schedule and tracking between all partners. The initial version will be available at project start; this plan will be updated regularly and the first issue officially submitted

Publications

Conference proceedings (6)

Suction and pulsed blowing for control of local wing-engine-slat-cut out flow separation: The INAFLOWT Project

Auteurs: Monat Shay, Maayan Posti, Bar Mizrahi, Ariel Yaniv, Avraham Seifert, Ofek Drori
Publié dans: AIAA AVIATION 2020 FORUM, 2020, ISBN 978-1-62410-598-2
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-2953

Suction and pulsed blowing for control of local wing-engine-slat-cut out flow separation: The INAFLOWT Project

Auteurs: Monat Shay, Possti Maayan, Junaid Ullah, Yaniv Ariel, Mizrahi Bar, Drori Ofek,, Seifert Avraham
Publié dans: Aerospace Europe Conference 2020 (AEC2020), 2020
Éditeur: Aerospace Europe Conference 2020 (AEC2020)
DOI: 10.5281/zenodo.4708647

NUMERICAL STUDY OF ACTIVE FLOW SEPARATION CONTROL FOR UHBR ENGINE INTEGRATION ON GENERIC WING IN HIGH-LIFT CONFIGURATION

Auteurs: Prachař, Aleš; Ullah, Junaid; Lutz, Thorsten; Ayele, Avi; Segal, Shaul
Publié dans: Aerospace Europe Conference 2020, 2020
Éditeur: Aerospace Europe Conference 2020
DOI: 10.5281/zenodo.4288432

Characterization of the Suction-and-Oscillatory-Blowing actuator by the hybrid RANS-LES CFD

Auteurs: Ales Prachar, Petr Vrchota
Publié dans: 2018 Flow Control Conference, 2018, ISBN 978-1-62410-554-8
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3375

Reynolds Number and Wind Tunnel Wall Effects on the Flow Field on a Generic UHBR Engine High-Lift Configuration

Auteurs: Junaid Ullah, Ales Prachař, Miroslav Šmíd, Avraham Seifert, Vitaly Soudakov, Thorsten Lutz, Ewald Krämer
Publié dans: Conference: 54th 3AF International, 2019
Éditeur: 3AF
DOI: 10.5281/zenodo.4284874

Active control of wing-engine-slat cut-out region flow separation

Auteurs: M. Possti, A. Yaniv, J. Ullah and A. Seifert (Tel-Aviv University/IAG Stuttgart)
Publié dans: Conference: 54th 3AF International, 2019
Éditeur: 3AF

Peer reviewed articles (2)

Reynolds number and wind tunnel wall effects on the flow field around a generic UHBR engine high-lift configuration

Auteurs: Junaid Ullah, Ales Prachař, Miroslav Šmíd, Avraham Seifert, Vitaly Soudakov, Thorsten Lutz, Ewald Krämer
Publié dans: CEAS Aeronautical Journal volume, Numéro 11, 2020, ISSN 1869-5582
Éditeur: Springer Science + Business Media
DOI: 10.1007/s13272-020-00463-w

Verification of Boundary Conditions Applied to Active Flow Circulation Control

Auteurs: Petr Vrchota, Aleš Prachař, Pavel Hospodář
Publié dans: Aerospace, Numéro 6/3, 2019, Page(s) 34, ISSN 2226-4310
Éditeur: MDPI
DOI: 10.3390/aerospace6030034

Book chapters (2)

Capability of RANS Simulations to Reproduce Flat Plate Boundary Layer Interaction with Suction and Oscillatory Blowing

Auteurs: Junaid Ullah, Nimrod Shay, Maayan Possti, Avraham Seifert, Thorsten Lutz, Ewald Krämer
Publié dans: New Results in Numerical and Experimental Fluid Mechanics XII - Contributions to the 21st STAB/DGLR Symposium, Darmstadt, Germany, 2018, Numéro 142, 2020, Page(s) 630-640, ISBN 978-3-030-25252-6
Éditeur: Springer International Publishing
DOI: 10.1007/978-3-030-25253-3_60

Active Flow Separation Control on a Generic UHBR Engine High-Lift Configuration by Means of Suction and Oscillatory Blowing

Auteurs: Junaid Ullah, Shay Monat, Avraham Seifert, Thorsten Lutz, Ewald Krämer
Publié dans: Fundamentals of High Lift for Future Civil Aircraft - Contributions to the Final Symposium of the Collaborative Research Center 880, December 17-18, 2019, Braunschweig, Germany, Numéro 145, 2021, Page(s) 365-384, ISBN 978-3-030-52428-9
Éditeur: Springer International Publishing
DOI: 10.1007/978-3-030-52429-6_23

Other (1)

Active flow control of Wing-Engine-Slat cut-out flow separation using suction and pulsed blowing

Auteurs: Monat Shay, Possti Maayan, Junaid Ullah, Yaniv Ariel, Mizrahi Bar, Drori Ofek, Seifert Avraham
Publié dans: Israel Annual Conference on Aerospace Sciences, IACAS60, 2020
Éditeur: Israel Annual Conference on Aerospace Sciences, IACAS60