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

Información del proyecto

INAFLOWT

Identificador del acuerdo de subvención: 754307

DOI

10.3030/754307

Proyecto cerrado

Fecha de la firma de la CE 22 Mayo 2017

Fecha de inicio 1 Junio 2017

Fecha de finalización 30 Septiembre 2020

Financiado con arreglo a

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Coste total

€ 1 146 750,00

Aportación de la UE

€ 700 000,00

Coordinado por

TEL AVIV UNIVERSITY
Israel

CORDIS proporciona enlaces a los documentos públicos y las publicaciones de los proyectos de los programas marco HORIZONTE.

Los enlaces a los documentos y las publicaciones de los proyectos del Séptimo Programa Marco, así como los enlaces a algunos tipos de resultados específicos, como conjuntos de datos y «software», se obtienen dinámicamente de OpenAIRE .

Resultado final

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

Publicaciones

Conference proceedings (6)

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

Autores: Monat Shay, Maayan Posti, Bar Mizrahi, Ariel Yaniv, Avraham Seifert, Ofek Drori
Publicado en: AIAA AVIATION 2020 FORUM, 2020, ISBN 978-1-62410-598-2
Editor: 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

Autores: Monat Shay, Possti Maayan, Junaid Ullah, Yaniv Ariel, Mizrahi Bar, Drori Ofek,, Seifert Avraham
Publicado en: Aerospace Europe Conference 2020 (AEC2020), 2020
Editor: 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

Autores: Prachař, Aleš; Ullah, Junaid; Lutz, Thorsten; Ayele, Avi; Segal, Shaul
Publicado en: Aerospace Europe Conference 2020, 2020
Editor: Aerospace Europe Conference 2020
DOI: 10.5281/zenodo.4288432

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

Autores: Ales Prachar, Petr Vrchota
Publicado en: 2018 Flow Control Conference, 2018, ISBN 978-1-62410-554-8
Editor: 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

Autores: Junaid Ullah, Ales Prachař, Miroslav Šmíd, Avraham Seifert, Vitaly Soudakov, Thorsten Lutz, Ewald Krämer
Publicado en: Conference: 54th 3AF International, 2019
Editor: 3AF
DOI: 10.5281/zenodo.4284874

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

Autores: M. Possti, A. Yaniv, J. Ullah and A. Seifert (Tel-Aviv University/IAG Stuttgart)
Publicado en: Conference: 54th 3AF International, 2019
Editor: 3AF

Peer reviewed articles (2)

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

Autores: Junaid Ullah, Ales Prachař, Miroslav Šmíd, Avraham Seifert, Vitaly Soudakov, Thorsten Lutz, Ewald Krämer
Publicado en: CEAS Aeronautical Journal volume, Edición 11, 2020, ISSN 1869-5582
Editor: Springer Science + Business Media
DOI: 10.1007/s13272-020-00463-w

Verification of Boundary Conditions Applied to Active Flow Circulation Control

Autores: Petr Vrchota, Aleš Prachař, Pavel Hospodář
Publicado en: Aerospace, Edición 6/3, 2019, Página(s) 34, ISSN 2226-4310
Editor: MDPI
DOI: 10.3390/aerospace6030034

Book chapters (2)

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

Autores: Junaid Ullah, Nimrod Shay, Maayan Possti, Avraham Seifert, Thorsten Lutz, Ewald Krämer
Publicado en: New Results in Numerical and Experimental Fluid Mechanics XII - Contributions to the 21st STAB/DGLR Symposium, Darmstadt, Germany, 2018, Edición 142, 2020, Página(s) 630-640, ISBN 978-3-030-25252-6
Editor: 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

Autores: Junaid Ullah, Shay Monat, Avraham Seifert, Thorsten Lutz, Ewald Krämer
Publicado en: 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, Edición 145, 2021, Página(s) 365-384, ISBN 978-3-030-52428-9
Editor: 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

Autores: Monat Shay, Possti Maayan, Junaid Ullah, Yaniv Ariel, Mizrahi Bar, Drori Ofek, Seifert Avraham
Publicado en: Israel Annual Conference on Aerospace Sciences, IACAS60, 2020
Editor: Israel Annual Conference on Aerospace Sciences, IACAS60