Conference Agenda

Overview and details of the sessions of this conference. Please select a date or location to show only sessions at that day or location. Please select a single session for detailed view (with abstracts and downloads if available).

 
 
Session Overview
Session
A07_01: Aerodynamics, Boundary Layers
Time:
Tuesday, 17/September/2024:
2:30pm - 4:30pm

Session Chair: Markus Rütten, German Aerospace Center
Location: H03

C.A.R.L.-Central Auditorium for Research and Learning Claßenstr. 11 52072 Aachen

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Presentations
2:30pm - 2:45pm

A numerical and experimental approach to stall hysteresis on a two-element wingsail (YSA)

Antonia Hillenbrand1,2, Suharto Saha3, Jakob Kuttenkeuler1, Philipp Schlatter3,4

1KTH Royal Institute of Technology, Center for Naval Architecture, Stockholm, Sweden; 2AlfaWall Oceanbird, Tumba, Sweden; 3Friedrich-Alexander-Universität Erlangen-Nürnberg, Institute of Fluid Mechanics, Erlangen, Germany; 4KTH Royal Institute of Technology, FLOW, Dept. Engineering Mechanics, Stockholm, Sweden

Hillenbrand-A numerical and experimental approach to stall hysteresis-480.pdf


2:45pm - 3:00pm

Dynamics of optimally perturbed wing-tip vortices: beyond Crow instability (YSA)

Navrose Navrose1, Mohd. Suhail Naim1, Vincent Brion2

1Department of Aerospace Engineering, Indian Institute of Technology Kanpur, India; 2DAAA, ONERA, F-92190 Meudon - France, France

Navrose-Dynamics of optimally perturbed wing-tip vortices-1383.pdf


3:00pm - 3:15pm

Global instability in scramjet flow (YSA)

Donato Variale1,2, Nicolas Alferez2, Stefania Cherubini1, Jean-Christophe Robinet2

1DMMM, Politecnico di Bari. via Edoardo Orabona, 4, Bari, Italy; 2DynFluid Lab., Arts & Metiers Institute of Technology / CNAM, 151, Bd. de l’Hopital, 75013, Paris, France

Variale-Global instability in scramjet flow-330.pdf


3:15pm - 3:30pm

Transonic shock buffet unsteadiness towards onset and offset conditions (YSA)

Christopher Julian Schauerte, Anne-Marie Schreyer

Institute of Aerodynamics, RWTH Aachen University

Schauerte-Transonic shock buffet unsteadiness towards onset and offset conditions-935.pdf


3:30pm - 3:45pm

A Unified Thermodynamic/Vortical Far-Field Force Method

Mauro Minervino1,2, Renato Tognaccini2

1CIRA S.C.p.A., Italian Aerospace Research Centre; 2University of Naples Federico II

Minervino-A Unified ThermodynamicVortical Far-Field Force Method-650.pdf


3:45pm - 4:00pm

Development of a hybrid inviscid model for airfoils in unsteady flows

Julien Deparday1, Samuele Stefanini2, Filippo Coletti2, Sarah Barber1

1OST-Eastern Switzerland University of Applied Sciences; 2Swiss Federal Institute of Technology (ETH Zürich)

Deparday-Development of a hybrid inviscid model for airfoils-504.pdf


4:00pm - 4:15pm

Aerodynamic characterisation of isolated cycling wheels using load and flow field measurements

Jiaqi Mao1, Peng Zhou1, Wei Yi2, Xin Zhang1

1Department of Mechanical and Aerospace Engineering, The Hong Kong University of Science and Technology, Clear Water Bay, Kowloon, Hong Kong, China; 2CAE & NVH Performance Development Center, BYD Auto Industry Co., Ltd., No.3009, BYD Road, Pingshan District, Shenzhen, Guangdong, China

Mao-Aerodynamic characterisation of isolated cycling wheels using load and flow field-231.pdf


4:15pm - 4:30pm

Electroactive morphing of an A320 wing prototype through traveling wave actuation for aerodynamic performance increase at high Reynolds number

Jacques Abou Khalil1,3, Rajaa El Akoury1, Clément Rouaix1,4, Abderahmane Marouf2, Yannick Hoarau2, Horia Hangan4, Jean-François Rouchon3, Marianna Braza1

1CNRS - IMFT; 2University of Strasbourg; 3INPT-LAPLACE; 4Ontario Tech

Abou Khalil-Electroactive morphing of an A320 wing prototype through traveling wave actuation-1262.pdf


 
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