PRELIMINARY AGENDA
4th EASN Association International Workshop
on Flight Physics & Aircraft Design
27th - 29th October 2014
Aachen, Germany
Time
Monday 27.10.2014
Room:
Generali
9:00
12:00
BoD Meeting
12:00
14:00
EASN General Assembly
13:00
14:00
Registration
14:00
14:30
Welcome and Introduction
E. Stumpf RWTH Aachen University, Prof. Schmachtenberg Rector of RWTH Aachen University , Sp. Pantelakis EASN Chairman,
W. Schröder RWTH Aachen University
14:30
15:00
Keynote Lecture:
"Aeronautics Research & Innovation at European Level - Achievements and Future Perspectives”,
Dr.-Ing. Dietrich Knoerzer, European Commission, DG Research-H.3 Aeronautics
15:00
15:30
15:30
16:00
Keynote Lecture:
"TBC",
Prof. Henke, Executive Board Aeronautics, DLR
Coffee
Monday 27.10.2014 (afternoon)
Generali
Time
Room:
Ford
Session
#1 Aircraft Structure Concepts & Design
#2 Aircraft Design Methodologies I
Session Chair(s)
C. Huehne / D. Scholz
B. Nagel
Aircraft Design for Future Operations,
V. Gollnick
PoLarBEAR Project:
16:00
16:25
Anisogrid Structures in EU-Projects ALaSCA and
PoLaRBEAR,
C. Hühne, S. Niemann
Junkers
#3 Flow and Load Control &
Atmosph. Turbulence
F. Scarano
Optical Inspection Tool for Micro-structured, Fuel
-Conserving Surfaces,
H. Brüning, K. Brune, Y. Wilke, G. Patzelt, M. Imlau,
J. Tschentscher, S. Hochheim
PoLarBEAR Project:
16:25
16:50
16:50
17:15
17:15
17:40
Recent Developments in the CEASIOM FramePEL-SKIN Project:
work Using the Common Language CPACS, A Novel Kind of Surface Coatings in Aeronautics
Development of lattice concept for robust
A. Da Ronch, J. Vos, A. Rizzi
composite fuselage structures,
- Overall Presentation,
V. Vassiliev, A.Shanygin, A. Razin, I. Kondakov
C. Brücker
Overview
of
the
Versatile
Options
to
Define
PoLarBEAR Project:
Future Wings Project:
Fuselage Structures within the CPACS Data Study of Passive and Active Deformation BehavEfficient modelling and analysis of anisogrid
Format,
fuselage structures,
iors of Hybrid Specimens Made of Composite
J. Scherer, D. Kohlgruber
Substrates and MFC Piezoelectric Patches,
T. Ludwig, R. Wagner
M. Chiarelli, V. Binante, M. Cagnoni, A. Massai, J.
Kunzmann, A. Cortebaldo, D. Romano
Transonic Wind-tunnel Investigation for Active
PoLarBEAR Project:
PyPAD:
Energy Approach for Analysis of Delamination A Multidisciplinary Framework for Preliminary Load Control Using a Winglet – Rudder – Configuration and for Passive Load Control Integrating
of Lattice Ribs,
Airframe Design,
Vortex Generators on the Wing Surface,
E.Dubovikov , V. Fomin
L. Travaglini, S. Ricci, G. Bindolino
TBC
18:05
Parametric Model Generation and Automated Impact of Certification Constraints in a MultiSizing Process for the Analysis of Aircraft Strucdisciplinary Design Process,
tures,
P. Schmollgruber, N. Bartoli, Y. Gourinat
T. Führer, S. Freund, F. Heinecke, C. Willberg
18:05
18:30
Automated Sizing of a Composite Wing for the
Usage within a Multidisciplinary Design Process,
T. Bach, T. Führer, S. Freund, C. Willberg, S.
Dähne
18:30
19:30
Airbus Student Information
19:00
21:00
17:40
Multi-Fidelity Mass Estimation of a Strutbraced Wing Configuration,
D. Böhnke, F. Dorbath, B. Nagel
Reception in Exhibition Area
END OF DAY 1
STARLET Project:
Wing-load Control via Fluidic Devices,
J. Sznajder, W. Stalewski
Aeronautics Lidar applications - Airborne LIDAR
detection of Clear Air Turbulence (CAT) within
the FP7 DELICAT project,
P. Vrancken, G. Ehret, M. Wirth, H. Barny, H. Veerman, L. Lombard
Time
Room:
Tuesday 28.10.2014
Generali
Registration
8:00
8:30
8:30
9:00
Keynote Lecture: Simplified Hybrid Laminar Flow Control, Geza Schrauf, Airbus Operations GmbH
9:00
9:30
Keynote Lecture: The present and the perspective of aerodynamic experimentation – the view of an operator of wind tunnels,
Prof. Dr.-Ing. Georg Eitelberg, Director of the German-Dutch Wind Tunnels
9:30
9:45
EASN AWARD introduction and presentation, Prof. Pantelakis
9:45
10:15
(Award) Lecture: The Air Transport System as Basis for Aircraft Design, Prof. D. Schmitt
10:15
10:30
Room:
Session
Ford
Coffee
Generali
#4 Morphing Aircraft Concepts
#5 Innovative AC Propulsion Concepts
Session Chair(s)
S. Ricci / A. Suleman
M. Hornung
Multi-disciplinary design investigations of propulsive fuselage aircraft concepts,
Application of Morphing Camber Concept to a
J. Bijewitz, A. Seitz, M. Hornung
Regional Aircraft,
A. De Gaspari, S. Ricci, A. Antunes, F. Odaguil, G.
Lima, M. Morelli
Hybrid Propulsion and Future Configurations,
NOVEMOR Project:
TBC
Design and Experimental Validation of Morphing
Wings,
J.E.Cooper, R. Cheung, C. Wales, L. Lambert, A.
Dale, J. Yang
Novel Air-Breathing Plasma Jet Propulsion for
NOVEMOR Project:
High Altitude Flight Platforms,
Multidisciplinary Design Optimization of Novel
B. Göksel, I. Mashek , H. Klefenz
and Morphing Aircraft Configurations: Computational Studies and Experimental Validation,
J. Vale, F. Afonso, F. Lau, A. Suleman, A. Antunes,
F. Odaguil, J. Parizi, J.E. Cooper
NOVEMOR Project:
10:30
10:55
11:20
10:55
11:20
11:45
NOVEMOR Project:
12:05
Plasma Flyer - The World's First Plasma Flow Controlled Flying Wing,
Geometry Modeling, Parametrization and MeshB. Göksel, H. Klefenz
ing of Conventional and Joined-Wing Aircraft,
M. Zhang, A. Rizzi, R. Nangia
NOVEMOR Project:
ANULOID Project:
12:05
12:30
Morphing Leading Edges for a Wing and Wingtip
Based on Compliant Structures,
S. Vasista, H.P. Monner, A. De Gaspari, S. Ricci
CFD Analysis and Optimization of Novel VTOL
Aircraft “Anuloid” in Relation to Vertical Flight,
Z. Janda
12:30
13:30
11:45
Lunch
Junkers
#6 Wake Vortex
E. Coustols
Enhanced Wake Vortex Decay in Ground
Proximity Triggered by Plate Lines,
F. Holzäpfel, A. Stephan, T. Heel, S. Körner
Multi-Model Ensemble Wake Vortex Prediction,
S. Körner, F. Holzäpfel, N. Ahmad, F. Proctor
Revisiting Wake Vortex Mitigation by Means
of Passive Devices: Demonstration and Validation of a Novel Device,
R. M. Buffo, E. Stumpf
Numerical Simulation of Vortex Roll-Up Processes at Elliptical Wings Using ReynoldsStress-Models,
A. Pongs, S. Braun, E. Stumpf,
Co-Rotating Vortex Interaction,
A. Romeos, A. Giannadakis, K. Perrakis, Th.
Panidis
Time
Room:
Session
Session Chair(s)
13:30
13:55
14:20
14:45
15:10
13:55
14:20
Ford
Tuesday 28.10.2014 (afternoon)
Generali
Junkers
#7 Innovative AC Configurations
#8 Aircraft Design Methodologies II
#9 Aeroelasticity & #10 Flight Dynamics
M. Meussen
E. Costa / P. Arbez
A. Dafnis / T. Panidis
RBF4AERO Project:
Investigation on Nonlinear Transonic Aeroelasticity using a Harmonic Balance Method,
S. Marques, R. Hayes, W. Yao
Three Surface Aircraft (TSA) Configuration –
Profits and Problems,
T. Goetzendorf-Grabowski, T. Antoniewski
New Small Aircraft Concepts and Required
Technologies Following FlightPath 2050 and Single European Transport Area,
K. Piwek, W. Wisniowski
14:45
Evaluation of Variable Camber Concept for Aircraft in Formation Flight,
Y. Liu, F. Peter, E. Stumpf
15:10
Design Challenges for Novel Concept of Highly
Manoeuvrable Flying Target,
Z. Goraj, A. Frydrychewicz
15:35
15:35
16:00
16:00
16:30
Innovative Benchmark Technology for Aircraft
Engineering Design And Efficient Design Phase
Optimisation
RBF4AERO Project:
SARISTU Project:
Technical Presentation 1
TBC
Effects of Flight Mechanics Model Simplification
in a State Space Aeroelastic Model for Loads
Analysis,
B. Prananta, R. Huls, H. van Tongeren, T. Kanakis
RBF4AERO Project:
Dynamics Properties Of Light Turboprop Aircraft
Including Weak And Strong Gyroscopic Effects,
E. Cichocka, Z. Goraj
Technical Presentation 2
TBC
TOICA Project:
Preliminary Flyability Analysis of Novel VTOL Aircraft "Lenscopter”,
Thermal Overall Integrated Conception of AirZ. Janda
craft - Overall Presentation (Part A),
P. Arbez
MAAT Project:
TOICA Project:
Cruiser-Feeder Airship Optimization and Modular Design,
M. Trancossi, M. Madonia
Thermal Overall Integrated Conception of Aircraft - Overall Presentation (Part B),
P. Arbez
Small UAV Autopilot System Synthesis, Tests and
Results,
S. Levin, A. Ledovskiy, R. Murzagalin, N. Ageev,
V. Kobtsev
SOAR Project:
Towards Deployment of the Lattice Boltzmann
Approach into the Aircraft Design Process,
E. Fares
A Novel Control Concept for Multirotor RPAS for
Stable Hovering Flight,
B. Messnarz, G. Loos
An Analysis of FanWing Flight Physics and Potential Business Cases,
J. Gibbs, G. Seyfang, P. Peebles, L. Villafane,
B.H. Saracoglu, G. Paniagua, C. May, B. Nagel,
A. Bachmann
Coffee
Time
Room:
Ford
Tuesday 28.10.2014 (afternoon)
Generali
Session
#11 Transition & #12 Advanced CFD
#13 Aerodynamic Wing Concepts & Design
#14 Innovative Cockpit Design &
#15 Personal Air Vehicle
Session Chair(s)
P. Doeffer / D. Drikakis
A. Rizzi / A. Seifert
R. Habig / F. Nieuwenhuizen
TFAST Project:
16:30
16:55
17:20
17:45
18:10
16:55
Multifunctional Moveables – from A350 into the
future,
Transition Location Effect on Shock Wave
D.
Reckzeh
Boundary Layer Interaction– Project overview,
P. Doeffer
TFAST Project:
DESIREH Project:
17:20
Numerical Simulations of Transitional Shock
Boundary Layer Interaction and Buffeting Control,
G. Barakos
Low Speed Design of Laminar Wings,
TBC
TFAST Project:
17:45
Physical and Experimental Challenges,
J.P. Dussauge
Hybrid Laminar Flow Implementation,
K. Risse
18:10
18:35
i-VISION Project:
i-VISION (Immersive Semantics-based Virtual
Environments for the Design and Validation of
Human-centred Aircraft Cockpits) – Overall
Presentation
L. Rentzos
i-VISION Project:
i-VISION – the Future of Human-centric Cockpit
Design,
R. Habig, L. Rentzos
MYCOPTER Project:
myCopter – Enabling Technologies for Personal
Aerial Transportation Systems,
F. Nieuwenhuizen, H. Bülthoff
Azure: High-Order CFD Software for Aerospace
AFLONEXT Project:
MYCOPTER Project:
Applications,
2nd Generation Active Wing Active Flow- Loads Vision Based Control And Navigation For PerD. Drikakis, A. Antoniadis, P. Tsoutsanis
& Noise control on Next Generation Wing sonal Aerial Vehicles,
Overall Presentation,
M. Achtelik, S. Lynen, S. Weiss, M. Chli, R. SiegA. Seifert
wart
Ground Testing: Driving Forward Innovation in
Fluid Dynamics,
K. Kontis
UMRIDA Project:
MYCOPTER Project:
Uncertainty Management for Robust Industrial
Design in Aeronautics - Overall Presentation
TBC
Handling Qualities and Training Requirements
for Personal Aerial Vehicles,
M. Jump, P. Perfect, L. Lu, M. White
END OF DAY 2
20:00
Junkers
22:00
* Facultative Dinner Description & Details.
Facultative Dinner *
Time
Room:
Wednesday 29.10.2014
Generali
Registration
8:30
9:00
9:00
9:30
Keynote Lecture: The Stratosphere challenges to Aeronautics & Space R&T,
Dr. Giovanni Bertolone, Chairman of the Italian Cluster for Aerospace Tecnology (CTNA)
9:30
10:00
Keynote Lecture:
Clean Sky projects on Aircraft Design and Flight Physics,
Giuseppe Pagnano, Coordinating Project officer – Clean Sky Joint Undertaking
10:00
10:30
Room:
Session
Ford
Coffee
Generali
Junkers
#16 Collaborative Support Actions I
#17 Cycloidal Rotor Configurations
#18 Air Transport Innovation & Policy
Session Chair(s)
D. Knoerzer
J.C. Páscoa / M. Schwaiger
E. Blanvillain / C. Galinsky
CROP Project:
HIKARI Project:
CAPPADOCIA Project:
10:30
10:55
Coordination Action Pro 'Production, Avionics,
Design' on Cost-efficiency in Aeronautics Overall Presentation,
F. Marty
Multi-Dielectric Barrier Discharge Plasma Actu- HIKARI: Joining Efforts to Pave the Way Towards
ators for Cycloidal Rotor Active Flow Control
High Speed Transport,
C.M. Xisto, J.C. Páscoa, J.A. Leger, A. Gerlach,
E. Blanvillain
CATER Project:
CROP Project:
HIKARI Project:
11:20
Coordinating Air transport Time Efficiency Research - Overall Presentation,
A. Napolitano
Cycloidal Rotor Aerodynamic and Aeroelastic
Analysis,
L. Gagon, G. Quaranta, M. Morandini, P. Masarati
Technical Presentation 2
TBC
OPTICS Project:
CROP Project:
TERESA Project:
11:45
Observation Platform for Technological and Institutional Consolidation of research in Safety Overall Presentation
B. Kirwan
D-Dalus - a Revolutionary VTOL Aircraft,
M. Schwaiger, S. Elflein, D. Wills
IATA’S Technology Roadmap and its Connection to Current Aviation Research and Innovation,
P. Nolte, T. Rötger
FORUM AE Project:
CROP Project:
REPAIR Project:
12:10
Forum on Aviation and Emissions,
O. Penanhoat
Optimized Pitching Schedules for a Cycloidal
Rotor in Hovering,
D. Angeli, A. Andrisani, A. Dumas
Future RepAIR and Maintenance for Aerospace
industry - Overall Presentation,
J. Pottebaum
CROP Project:
12:35
12:35
Coordinating research and innovation in the
field of Aeronautics and Air Transport: Overview
and latest achievements of running CSAs
Discussion & Feedback
Responsiveness of European Airline Business
Stakeholders Regarding the Inclusion of Aviation in the ETS,
M. Naumow, P. Nolte
12:30
13:30
10:55
11:20
11:45
Aerodynamic Optimization of Cyclorotors,
J.A. L. Monteiro, J.C. Páscoa, C. M. Xisto
Lunch
Time
Room:
Ford
Wednesday 29.10.2014 (afternoon)
Generali
Junkers
Session
#19 Collaborative Support Actions II &
#20 Noise
#21 MDO & #22 Aerodynamic Optimisation
#23 Cabin Technology & #24 Out-of-the-Box
Concepts & #25 Improved GVT
Session Chair(s)
G. Bugeda /E. Stumpf
J. Pons i Prats/W. Schröder
G. Cabañero / Z. Goraj
PROMOAIR Project:
ESPOSA project:
IN-LIGHT Project:
13:30
13:55
Promoting Aeronautics Innovation and Research - Overall Presentation,
A.Chamos
GRAIN2 Project:
13:55
14:20
14:45
15:10
15:35
MDO Approach for a Light Turboprop Aircraft - Innovative bifunctional aircraft window for lightEngine Integration and Improvement,
ing control to enhance passenger comfort,
A. Iwaniuk, W. Wisniowski
G. Cabañero, A. Viñuales
ESPOSA project:
14:20
GReener Aeronautics International NetworkingAerodynamic Design of Engine Intake Duct
2 - Overall Presentation,
Shape of a General Aviation TurboProp Aircraft,
G. Bugeda
B. Soemarwoto, O. Boelens, T. Kanakis
14:45
Can Constructal Theory Help in Overcoming the
X-NOISE Project:
Aviation Noise Research Network and Coordi- Intrinsic Limits and Simplifying the Processes by
MDO?,
nation,
M.
Trancossi
D. Collin
Investigations on Drag Reduction for a Light
Class Utility Helicopter,
C. Breitsamter, M. Grawunder, R. Reß
IN-LIGHT Project:
Technical Presentation 2
TBC
IN-LIGHT Project:
Technical Presentation 3
TBC
Airport based air stream assistance for aircraft
take off and landing,
P. Nikolakopoulos, D. Bompos, D. Drikakis
15:10
Discussion & Feedback
15:35
Psycho Acoustic Optimization,
A. Sahai,
Aerodynamic Optimisation Using CAD Parame- One Method of Spatial Flight Path Optimization
terisations in SU2,
for Non-Stationary Aircraft Flight Regimes,
S. Marques, P. Hewit, T. Robinson
S. Levin
16:00
Long-Range Noise Propagation of Aircraft
Noise,
A. Filippone
Minimization of Body of Revolution AerodynamCESAR Project:
ic Drag at Supersonic Speeds in the Framework Model Updating of Small Aircraft Dynamic Finite
of RANS,
Element Model Using Standard Finite Element
N. Ageev, A. Pavlenko
Software,
B. Prananta, T. Kanakis, J. Vankan
END OF DAY 3
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