News and Events
First workshop material
EventsPublications & presentationsPublications & presentations 5th October, 2015
Free presentations download available of this unique day !
The AFLoNext project held its first specialised Workshop on Hybrid Laminar Flow and Active Flow control, noise and load control, on September 10, 2015. This took place in the TUDelft premises, in conjonction with CEAS 2015.
Session 4: "Vibrations mitigation / control in undercarriage area”
Session 5: "Noise reduction on flap and undercarriage”
Conclusions - Martin Wahlich Aribus Operations GmbH
The primiry aim of this one-day event was to offer its participants a forum, encouranging open exchange of information with fellow members and present the latest advancements of each of the 6 project technology streams.
Thus, the event proved to be a unique opportunity for the participants to obtain an overview of the recent achievements on the research scene, with 18 presentations from participating organisations. Furthermore, the workshop attendees had the opportunity to engage into fruitful discussions and networking with more than 50 representatives of academia, research community and industry involved in AFLoNext. Finally, the 2 key-note presentations from distinguished individuals gave a clear insight on the future industrial trends and European priorities with respect to the medium and long-term goals, as set by the aviation stakeholders, positioning the project on the relative technology trajectory and showing the connection with Clean Sky 2. About 100 participants had registered to the event.
The different presentations can be downloaded below:
Key note lecture no. 1: Stepless and sustainable research for the aircraft of tomorrow- From AFLoNext to Clean Sky 2 by Markus Fischer Airbus Operations GmbH
Key note lecture no. 2: On the development of practical active flow control technologies – as pirations and realities by Clyde Warsop BAE Systems
Session 1 : “Hybrid Laminar Flow Control on wing and fin”
Overview on the HLFC activities in AFLoNext and beyond: Geza Schrauf Airbus Operations GmbH
Aerodynamic design of an HLFC leading edge for a VTP:Heiko v. Geyr Deutsches Zentrum Fuer Luft- Und Raumfahrt EV, DLR
Structural design of an HLFC leading edge for a VTP:Stéphane Debaisieux Societe Nationale De Construction Aerospatiale Sonaca SA
Integrated HLFC design for the leading edge of a wing:James Aldermann Airbus Group Ltd, Alan Mann Airbus Defence and Space GmbH
Preliminary Krüger design for an HLFC wing: Jochen Wild Deutsches Zentrum Fuer Luft - Und Raumfahrt EV, DLR
Session 2: “Active Flow Control on outer wing” and “Active Flow Control on wing / pylon"
Strake Vortex Interaction with Active Flow Control Applied at the Engine/Wing Junction: Sebastian Fricke, Vlad Ciobaca, Jochen Wild, Anna Kröhnert Deutsches Zentrum Fuer Luft - Und Raumfahrt EV, DLR and Olivier Blesbois Airbus Defence and Space GmbH
Aerodynamic Design and System Development of Synthetic Jet Actuation for Flow Control at the Engine/Wing Junction: Harmen Schippers Stichting Nationaal Lucht- En Ruimtevaartlaboratorium, NLR, Martin Schueller Fraunhofer-Gesellschaft Zur Foerderung Der Angewandten Forschung EV , Bruno Stefes Airbus Operations GmbH, Theo ter Meer Stichting Nationaal Lucht- En Ruimtevaartlaboratorium, NLR, Perez Weigel Fraunhofer-Gesellschaft Zur Foerderung Der
Angewandten Forschung EV, Petr Vrchota Vyzkumny A Zkusebni Letecky Ustav A.S., VZLU, Stefan
Wallin Totalforsvarets Forskningsinstitut, FOI, Michael Meyer Airbus Defence and Space GmbH
Characterisation of baseline flow on outer wing region for numerical sizing of AFC concepts: Petr Vrchota Vyzkumny A Zkusebni Letecky Ustav A.S., VZLU, Alan Mann Airbus Defence and Space GmbH, Simone Crippa Airbus Operations GmbH, Pierluigi Ianelli Centro Italiano Ricerche Aerospaziali SCPA, CIRA, Vlad Ciobaca, Jochen Wild Deutsches Zentrum Fuer Luft - Und Raumfahrt EV, DLR, Peter Wong Aircraft Research Association Limited, ARA, Jean-Luc. Hantrais-Gervois Office National D'etudes Et De Recherches Aerospatiales, ONERA, Jean-Pierre Rosenblum Dassault Aviation SA.
Numerical sizing of Active Flow Control concepts on the outer wing: Jean-Pierre Rosenblum Dassault Aviation SA, Petr Vrchota Vyzkumny A Zkusebni Letecky Ustav A.S., VZLU, Stefan Wallin Totalforsvarets Forskningsinstitut, FOI, Pierluigi Iannelli Centro Italiano Ricerche Aerospaziali SCPA, CIRA, Vlad Ciobaca, Jochen Wild Deutsches Zentrum Fuer Luft - Und Raumfahrt EV, DLR, D. Norman, Jean-Luc. Hantrais-Gervois Office National D'etudes Et De Recherches Aerospatiales, ONERA, Manfred Schneider Airbus Defence and Space GmbH
Session 3: "Active Flow Control on wing trailing edge”
Computational Fluid Dynamics, results and outlook: Petr Vrochta, Vyzkumny A Zkusebni Letecky Ustav A.S., VZLU,
Computational Fluid Dynamics, results and outlook: Petr Vrochta, Vyzkumny A Zkusebni Letecky Ustav A.S., VZLU,
SaOB/supercritical coanda device, current development and outlook: Avi Seifert, Tel Aviv University
Session 4: "Vibrations mitigation / control in undercarriage area”
Computational Fluid Dynamics results and outlook on Flight Test: Arthur Rizzi (Kungliga Tekniska Hoegskolan, KTH)
Finite Element Model, Ground Vibration Test and outlook on Flight Test: Pascal Lubrina (Office National D'etudes Et De Recherches Aerospatiales, ONERA)
Session 5: "Noise reduction on flap and undercarriage”
Overview of the aeroacoustic activities in AFLoNext and related contributions to flight testing: Michael Bauer (Airbus Defence and Space GmbH)
Computational Fluid Dynamics based gear-wake flap flow interaction analysis: Alexander Büscher (Airbus Operations GmbH)
Analysis of acoustic wind tunnel test in the NWB for gear-wake flap interaction: Michael Pott-Pollenske (Deutsches Zentrum Fuer Luft - Und Raumfahrt EV, DLR)
Experimental results from AWB wind tunnel test on porous flap side edge for an A320 flap geometry: Johann Reichenberger (Airbus Defence and Space GmbH
Conclusions - Martin Wahlich Aribus Operations GmbH
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Finally, AFloNext will be present during Aerodays (Stand 05-08, Flight Physics) , Come visit us, we look forward to meeting you there !
