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Tuesday 25Th February 2020 Tuesday 25th February 2020 8:30 REGISTRATION / WELCOME 09:00 - 10:10 PLENARY SESSION 1 - OPENING Chair: Christian Mari (Chair of AEC2020) Welcome by Louis le Portz & Michel Scheller, 3AF Presidents Alain Rousset, "Nouvelle Aquitaine" Region President 10:10 - 10:40 COFFEE BREAK ANERS AERONAUTICS SPACE Auditorium A R01 (G1+G2) R02 (D1+D2) R03 (F1) R04 (E1) R05 (E2) R06 (F2) R07 (H1) R08 (H2) Session 1 : ANERS Session 2 : Aerodynamic/Flow Control Session 3 : Hybrid/electric airplanes design and Session 4 : Composites manufacturing Session 5 : Research infrastructures for greener and Session 6 : CS Project BLADE Session 7 : Clean Space, Space Debris I Session 8: Materials and Advanced Manufacturing for Session 9 : Space Propulsion I Chair: Ph. Beaumier (ONERA) analysis tools Chair: L. Paletti (NLR) safer aviation Chair: V. Selmin (CS) Chair: G. Ortega (ESA) Space Application I Chair: J. Gonzalez del Amo (ESA) Chair: F. Boudjemaa (Safran) Chair: C. Nae (INCAS) Chair: K. Pfaab (CNES) 49 156 136 363 109 721 578 703 10:40-11:00 Symposium Introduction and Session Moderation: A Method for Estimating Drag Reduction A General Preliminary Sizing Procedure for Pure- Automated Fiber Placement based manufacturing of Towards the Multimodal Detection of Sleep in Pilots BLADE - Breakthrough Laminar Demonstrator in Aerodynamically stabilized origami-based drag sail Design of a MoonFibre Spinning Apparatus for the Multidisciplinary design optimization framework for John-Paul Clarke (UTC & Georgia Tech) Performance of Riblets Installed on Aircraft Surfaces Electric and Hybrid-Electric Airplanes carbon fiber reinforced sandwich shell parts B. BOHDAN, Honeywell, CZ Europe - An Overview A. ABRISHAMI, Tsinghua University, CN Use on a REXUS Research Rocket the conceptual design of hybrid rockets S.KOGA, Japan Aerospace Exploration Agency, JP L.TRAINELLI, Politecnico Di Milano, IT T. ZENKER, Fraunhofer, DE A. EBERLE,Airbus Operations, DE C. KRÄMER, Rwth Aachen University, DE F. AFONSO, Instituto Superior Tecnico, PT Symposium Opening Speeches: M. KYRIAKOPOULOS (European Commission) 247 514 503 106 424 592 017 497 11:00-11:20 Evaluation of Drag Reducing Paint-Riblet in Flight Optimization tool for equipment placement and Optimizing in-situ consolidation of xenon flashlamp Towards Validation of Scaled Flight Testing Clean Sky SFWA BLADE and Saab‘s integrated Ecodesign as a new lever to enhance your global Additive manufacturing of functionally graded Ignition of green propellant rocket thrusters using a M. KURITA,Japan Aerospace Exploration Agency, JP routing in more electric aircraft based automated fiber placement P. SCHMOLLGRUBER, ONERA, FR composite upper cover value proposition: from Space to Corporate ceramics with in-situ resources miniaturized high energy laser J. VANKAN, Nlr, NL D. DEDEN, DLR, DE K. KARLSSON, SAAB ab, SE K. LE BLEVENNEC, Vito, BE B. RICH, Esa/Estec, NL T. BERECZKI, Silicon Austria Labs Gmbh, AT 393 522 315 210 159 540 366 510 11:20-11:40 RT1: Research Networks Activity Reports Quantitative prescription of transonic-airfoil-buffet Sensitivity analysis of a hybrid-electric aircraft Automated Joining and Assembly of Thermoplastic A novel Aircraft Wing Inspection Framework based Highlights for natural laminar wing manufacturing Deorbiting Small Satellites from the ISS using a Development, manufacturing and testing of an AM Influence of Solution Conductivity on Electrolytic occurrence by persistent homology powertrain based on Sobol indices. Fuselage Structures for the Aircraft Factory of on Multiple View Geometry and Convolutional Neural developments Tethered System Flexible Hinge made by Laser Metal Deposition for Decomposition of HAN Aqueous Solutions C.KAZUHISA, The University Of Electro- M. PETTES-DULER, Laplace Lab, FR Tomorrow Network M. CASTILLO, Aernnova, ES A. VALMORBIDA, University Of Padova, IT Space Applications M-H. WU, National Cheng Kung University, TW ASCENT (USA) Communications, JP B. DIEHL, Fraunhofer Ifam, DE B. KUANG, Cranfield Universit, GB C. MELZER, Ruag Space, DE ECATS (EU) FORUM-AE (EU) X-NOISE / ANIMA (EU) ANNA (Int'l) 409 24 408 269 472 501 068 474 11:40-12:00 Investigation of base drag reduction on bodies of Uncertainty quantification of complex Generating durable hybrid Ti/CFRP adhesive joints Analysis of combined jet-perforated boundaries BLADE Flight Test Aircraft Conversion and Deployment Requirements for Deorbiting NdFeB magnets: main findings of the failure Characterisation of acoustically coupled flow field revolution implementing passive and active flow multidisciplinary aircraft systems for aerospace structures by laser pretreatment efficiency to solve the problem of the wind tunnel Innovative Instrumentation Electrodynamic Tether Technology investigation activity and development of alternative dynamics from high-speed imaging in a high control techniques A. HARISH, United Technologies Research Centre U. LOMMATZSCH, Fraunhofer Ifam, DE wall interference at transonic speeds A. VALMORBIDA, University Of Padova, IT approach based on 3D printed composite material pressure rocket thrust chamber C. BLIAMIS, Aristotle University of Thessaloniki, GR Ireland Ltd, IE A. VOLKOVA, TsAGI, RU T. FOL, Airbus, FR L. PIGLIARU, Telespazio Vega Uk For Esa, NL M. SON, DLR, DE Moderation: Dominique Collin (Safran) 471 411 588 22 266 328 259 525 12:00-12:20 A Review of Experiments on Control of Cross-flow Tool to predict and avoid Partial Discharges in stator Genetic optimization of stacking sequences for New long-range cabin mock-up enabling the BLADE Flight Test Instrumentation for Transition Using inflatable braking devices to remove space Topology Optimization Based Design of Secondary CO2 Based ISRU Propulsion for Satellites and Disturbances Using Dielectric Barrier Discharge slot of rotating motors fed by inverter laminated composite structures with ply drops simulation of flight cases my means of tempered Detection debris from orbit in the orbital service system and Tertiary Structures of the ORION-MPCV Spacecrafts in the Vicinity of Mars D. SBOEV, TsAGI, RU P. COLLIN, Laplace, FR A.F. CORTESI, Scalian, FR fuselage elements S. KOCH, DLR, DE application European Service Module C. BERENGUER, Dedalos Ltd, GR P. LANGE, DLR, DE M. HERMOSILLA, School Of Aeronautical And Space G. RODRIGUES, ESA/ESTEC, NL Engineering, Technical University Of Madrid, ES 709 507 606 698 603 018 523 12:20-12:40 Ongoing progress in Flow Control Actuators and Electrothermal Models and Design Approach for High Design and manufacturing maturation of a Icing test of propellers for multi-rotary URAV BLADE flight test: impact of noise on the laminar ADEO - The European Commercial Passive De-Orbit ISRU Technology Propulsion for Missions in the required electronics Specific Power Electric Motor for Hybrid Aircraft Thermoplastic Composite Keel-beam M. YAMASAKI, Kanagawa Institute Of Technology, JP turbulent transition Subsystem Family Enabling Space Debris Mitigation Solar System G. AIGOUY, Cedrat Technologies, FR S. TOUHAMI, Laplace Laboratory, FR L. ANGEL, Eurecat Tech Center, ES O. VERMEERSCH, ONERA, FR M. KOSMASLKI, Hps Gmbh, DE K. KATSONIS, Dedalos Ltd, GR 12:40 - 14:00 LUNCH 14:00 PLENARY SESSION 2 Chair: Christophe Hermans, DNW KEYNOTE SPEECH 1: The space climate observatory : a green new deal, Jean-Yves le Gall, CNES President KEYNOTE SPEECH 2: "Clean Sky: towards climate-neutral aviation", Axel Krein, Executif Director Clean Sky JU 15:00 Session title Session 10: NOISE IMPACTS Session 11 : Aerodynamic /Aircraft performance Session 12 : Hybrid/electric Thermal management Session 13 : Composites analysis & modelling Session 14 : Numerical Simulation and Optimization Session 6 Cont'ed: CS Project BLADE Session 15 : Clean Space, Space Debris II Session 16 : Environmental Control and Life Support Session 17 : Space Propulsion II ANIMA Special Session Chair: L. Campos (IST) Chair: C. M. Margariti (CS) Chair: V. Guénon (Safran) of Novel Aircraft Concepts Chair: V. Selmin (CS) Chair: C. Huehne (DLR) in Space Chair: V. Fernandez (ESA) Moderation: Karl Bolin (KTH) Chair: I. Dimino (Cira) Chair: R. Bureo (ESA) 66 317 498 631 65 184 044 602 154 15:00-15:20 An overview of ANIMA’s achievements on aviation Simulations of Light Aircraft Spin Maneuvers Evaluation of a new OGV architecture for an Micromechanical analysis of fibre-reinforced Numerical Investigation of the Effects of Fuselage BLADE - Natural Laminar Flow Flight Testing For a cleaner space, the de-orbiting approach of the Containment of Hazardous Materials for Human Hypergolicity and ignition delay study of green impact management L. BOVET, Elisa Aerospace, FR enhanced energy dissipation composites with microstructural defects via a Upsweep in a Propulsive Fuselage Concept T. GIBSON, Airbus, GB PROBA P200 platform with the dragsail subsystem Spaceflight: A Simplified Approach to Verification for bipropellant system without catalyst L. LEYLEKIAN, ONERA, FR E. LAROCHE, ONERA, FR component-wise approach A.L. HABERMAN, Bauhaus Luftfahrt E.V., DE ADEO Sealed Hazardous Fluid Containers J. QUESADA MAÑAS, Delft University Of Technology, M. NAGARAJ, Politecnico Di Torino, IT R. ERNST, Qinetiq Space Nv, BE R. BUREO DACAL, European Space Agency, NL NL 137 625 415 677 484 730 352 116 168 15:20-15:40 Quality of Life: An expanded agenda of airport Wind tunnel aerodynamic investigation of quad plane Hybrid aircraft 2035: high performance cooling Improved damage prediction for woven composites Numerical low-fidelity method for improved analysis Towards Laminar Bizjets On the Need to Develop Research for
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