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

Deliverables

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

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Publications

Development and Verification of Simplified Boundary Condition of SaOB Actuator

Author(s): Vrchota, P.; Prachař, A.; Hospodář, P.; Dolgopyat, D.; Seifert, A.
Published in: March 2018: 58th Israel Annual Conference on Aerospace Sciences,, 2017

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

Author(s): Ales Prachar, Petr Vrchota
Published in: 2018 Flow Control Conference, 2018
DOI: 10.2514/6.2018-3375

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

Author(s): Junaid Ullah, Nimrod Shay, Maayan Possti, Avraham Seifert, Thorsten Lutz, Ewald Krämer
Published in: Conference: 21.STAB-Symposium, 2018

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

Author(s): Junaid Ullah, Ales Prachař, Miroslav Šmíd, Avraham Seifert, Vitaly Soudakov, Thorsten Lutz, Ewald Krämer
Published in: Conference: 54th 3AF International, 2019

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

Author(s): M. Possti, A. Yaniv, J. Ullah and A. Seifert (Tel-Aviv University/IAG Stuttgart)
Published in: Conference: 54th 3AF International, 2019

Verification of Boundary Conditions Applied to Active Flow Circulation Control

Author(s): Petr Vrchota, Aleš Prachař, Pavel Hospodář
Published in: Aerospace, Issue 6/3, 2019, Page(s) 34, ISSN 2226-4310
DOI: 10.3390/aerospace6030034