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 Asteroids’ Electrodynamic Centrifuge for Space Habitats with Development of a 100 mN Green Monopropellant responsibility? in transient state systems for power electronics converters under crush loading of breakthrough aero-propulsive systems T. DELILLE, Dassault Aviation, FR Deviation from the Collision Trajectories with Earth Artificial Gravity Thruster F. RAJE, Manchester Metropolitan University, GB A. TARNOWSKI, Wut, PL F. ACCORINTI, Isae-Ensma, FR R. LOMBARKIA, Université Laval, CA E. BENICHOU, Isae-Supaero, FR using Cannons with Artificial Gravitation P. JEVTOVIC, Orbis-Ip, ES A. SHCHETKOVSKIY, Plasma Processes, Llc, US C. SANDU, Incdt-Comoti, RO
Session 18 : On board energy management & Session 19: Hybrid/ Electric Propulsion and Aircraft Session 20 : Space Aero Thermo Dynamics Alternative Power Source Chair: G. Way (Rolls Royce) Chair: J.-L. Verant (ONERA) Chair: C. M. Margariti (CS)
15:40-16:00 146 123 383 607 152 679 574 131 A role for communication and engagement in a Forces on a 3.5:1 prolate spheroid in accelerated Testing of a compact and lightweight two-phase Exploitation of high performance composite Structural Topology Optimisation of a Gas Turbine Development of a Hybrid-Electric Propulsion System Study on Mitigation of Reentry Blackout by Surface Simulation and optimization of a control system for comprehensive approach to aircraft noise annoyance relative motion with a viscous fluid pumped cooling system with 3D printed aluminium structures at elevated temperatures Engine and Nacelle Integration Components for Unmanned Air Vehicles Catalysis Effects in Arc-Heated Wind Tunnel hybrid rocket engines (HRE) mitigation G. CARBONE, Flying Whales, FR components M. LIEBISCH, DLR, DE Employing A Medial Surface Representation F. AFONSO, Instituto Superior Tecnico, PT H. TAKASAWA, Hokkaido University, JP A. COSTANTINO, QinetiQ Space, BE G. HEYES, Manchester Metropolitan University, GB H. J. VAN GERNER, NLR, NL L. WANG, University of Southampton, GB
16:00-16:20 271 717 87 489 494 643 76 Aircraft Noise Management Practices in Eastern Analysis of photovoltaic cells for powering a solar Analysis of guided wave propagation in the CFRP Codesign of Aircraft Vertical Tail and Control Laws Next Stages in bringing Hybrid-Electric Power Effect of mass addition on heat transfer and Experimental investigation of flow regime transition European countries airplane and evaluation of the impact of subjected to moisture influence with distributed Electric Propulsion and Flight Systems for Aviation to life boundary layer stability of descent module for Mars for boiling hydrogen flow in horizontal pipes E-N. BURTEA, National Research And Development photovoltaics on the environment O.WIESLAW, Polish Academy Of Sciences, Institute Of Envelop Constraints G. WAY, Rolls-Royce Plc, GB exploration Y. SAKAMOTO, Jaxa, JP Institute For Gas Turbines Comoti, RO M. DUDZIAK, Agh University Of Science And Technology Fluid Flow Machinery, PL E. NGUYEN VAN, Isae, ONERA, FR Y. EGOROV, Central Aerohydrodynamic Institute, RU In Cracow, PL
16:20-16:50 COFFEE BREAK Session 10 Cont'ed : NOISE IMPACTS Session 21 : Aerodynamic/Laminarity Session 22: Green and safe systems & operations I Session 23 : Testing, monitoring & certification Session 24 : Numerical Simulation and Optimization Session 19 Cont'ed: Hybrid/ Electric Propulsion and Session 25 : Testing I Session 26 : Structures, Thermal and Mechanisms I Session 27 : Space Propulsion III ANIMA Special Session Chair: A. le Pape (ONERA) Chair: M. Bourgois (Eurocontrol) Chair: W. Ostachowicz (Polish Academy of Science) of Novel Aircraft Concepts Aircraft Chair: O. Pin (ESA) Chair: P. Corberand (Airbus Defence And Space) Chair: V. Fernandez (ESA) Moderation: Karl Bolin (KTH) Chair: M. Kyriakopoulos (EC) Chair: G. Way (Rolls Royce)
16:50-17:10 291 110 464 396 003 618 719 061 369 Exemplar case studies of aviation noise mitigation Studies of laminar-turbulent transition on large-scale Evaluation of Thermal Comfort for Novel Aircraft Digital Twin approach for critical components using Analytical Prediction of Heaving and Pitching Structure – system design interdependencies of Virtual Shaker Testing (VST) and its application to a Centrifugal pump breadboard design for a Thrust measurement system for propulsion of the strategies in the European Union transonic airfoil Cabin Ventilation Concepts PCRT Motions of Seaplanes hybrid-electric aircraft during conceptual design test item Mechanical Pumped Fluid Loop Cooling System satellite G. HEYES, Manchester Metropolitan University, GB V. SOUDAKOV, TsAGI, RU D. SCHMELING, DLR, DE T. KOEHLER, Vibrant Gmbh, DE J. MASRI, Northumbria University, GB phase D. PEDERBELLI, Polytechnic Of Turin, IT I-F. POPA, COMOTI, RO F. NICULESCU, COMOTI, RO A. BARDENHAGEN, Technische Universität Berlin, DE
17:10-17:30 343 128 473 706 575 331 287 031 365 Health impacts of aircraft noise exposure Comparison of Heating Methods for Transition Turbulence prediction for aircraft by means of high- Military Transport aircraft ditching certification from Static Aeroelastic Model Development for Folding Conceptual Design Studies of Hybrid Electric Low heat transfer and high load capacity attachment Vibro-Acoustic Response Prediction of the Effects of compounds in liquefied methane on rocket S. BENZ, Zeus Gmbh, DE Detection by TSP on a Generic Nacelle in the Pilot dynamic fifferential pressure measurements impact and floatation standpoint Winglet Design Propulsion Air Vehicles in the Frame of Clean Sky2 system for probes in aerospace testing facilities Bartolomeo Multi-Purpose Payload engine operation ETW A. GALFFY, Tu Wien, AT M. OLIVER-HERRERO, Airbus, ES B. SITOTAW KIDANE, University Of Bologna, IT Large Passenger Aircraft A. CANCESCU, Comoti, RO D. BINET, Hexagon | Free Field Technologies, BE E. GOOS, DLR, DE P. GUNTERMANN, Etw Gmbh, DE P. SCHMOLLGRUBER, ONERA, FR
17:30-17:50 348 538 556 713 368 596 462 673 121 Foundations for a comprehensive approach of Investigation of a sectioned boundary layer suction Designing and Maturating Doppler LIDAR Sensors Some challenges in aeroelasticity and their A multi-mode morphing flap for the next-generation The LCA60T, a 4-MW hybrid-electric propulsion A supersonic glider: fluid dynamics predictions and Design, Testing and Feasibility Analysis of a Novel A Dynamic Model for HTP Monopropellant Thruster: acoustic and non-acoustic measures of aircraft noise system in application to the three-dimensional for Gust Load Alleviation: Progresses Made Since experimental investigation towards a cleaner aviation regional aircraft airship free flight experiments analysis Docking Module for Small Satellites Simulation Results and Validation annoyance mitigation boundary layer laminarization on the swept wing AWIATOR A. LEPAGE, ONERA, FR F. AMOROSO, Unibersity Of Naples "Federico Ii", IT J. BERNARD, Flying Whales, FR M. ALBISSER, ISL, FR R. GAJENDRA PAREEK,Srm Institute Of Science And C. SUKMIN, Kaist, KR J. HAUBRICH, Zeus Gmbh, DE S. TOLKACHEV STEPAN, TsAGI, RU N. FEZANS, DLR, DE Technology, IN
17:50-18:10 92 506 634 075 173 450 005 286 Association between short-term annoyance and Laminar flow control along the wing leading edge Use of the DressMAN (Dummy Representing Suit for Numerical Analysis on Aerodynamic Characteristics Control systems, telemetry and battery management Automated testing for satellite on-board systems Qualification of two Phase Change Material Heat Modelling nitrous oxide dynamics in oxidizer tank, heart rate during aircraft noise exposure F. MÉRY, ONERA, FR Simulation of huMAN heat loss) measurement system of Box-Wing for Application to Flying Car system of AGH UST Solar Plane- Photovoltaic S. MANAP, Nazarbayev University, KZ Accumulators for the HEXAFLY Hypersonic glider feed line and injector of hybrid rocket engine B. OHLENFORST, Nlr, NL to assess normal and emergency operation thermal K. MARUYAMA, The University Of Electro- Unmanned Aerial Vehicle J-P. COLLETTE, Walopt, BE J. SZYMBORSKI, The Szewalski Institute Of Fluid-Flow cases in the Business-Jet Cabin Mock-Up. Communications, JP J. GAJDA, AGH UST, PL Machinery Polish Academy Of Sciences, PL V. NORREFELDT, Fraunhofer Ibp, DE
18:10-18:30 532 655 744 535 554 359 082 321 Aircraft noise exposure and impact assessment and Numerical and experimental studies on the concept ReMAP – An Integrated Fleet Health Management A Framework for the Development of a Full-size A Comparative study of High and Low Fidelity Application of functional analysis and spectral Evaluation criteria of stress intensity factor at the A thermo-mechanical analysis with the use of tasks management of short/medium range aircraft with natural laminar solution for Condition-based Maintenance in Aviation Aircraft Morphing Winglet Propulsion Models for Hybrid Electric Aircraft decomposition for frequency dependent selection of interface corner under mechanical loading in a non-linear formulation for a low-thrust thruster O. ZAPOROZHETS, National Aviation University, UA flow wing B. SANTOS, TU Delft, NL J. XI, Ryerson, CA V. PALLADINO, Atr Aircraft, FR control sensors in direct field environmental acoustic F. MAAMAR, Génie Mécanique, DZ calculations during lifetime prediction with the SPT- N. PUSHCHIN, TsAGI, RU tests 50 thruster as an example M. ALVAREZ BLANCO, Siemens Industry Software Nv, G. PARAKHIN, Fsue Edb Fakel, RU BE
18:30-18:50 483 216 733 600 633 059 064 A novel tool to estimate the impact - beyond Modeling of the static pressure distribution along an Multi-Physics Methodology for Phase Change Due to THEA-CODE: a design tool for the conceptual design A hybrid real time model for integrating TVC Design and testing of a closing and sealing system SWAN sandwich nozzle program for Ariane 6, acoustics - of aircraft noise on airport communities airfoil Rapidly Depressurised Two-Phase Flows of hybrid-electric aircraft with conventional or subsystem in the new Vega-C HWIL: design-to-cost for a Phobos Sample Return mission qualification and maturation I. LEGRIFFON, ONERA, FR M. HASNAOUI, Royal Air Force School, MA V. EUSEBIO, Univerisad Politecnica De Madrid, ES unconventional airframe configurations development and validation R. MIHALACHE, COMOTI, RO L. BROX, Gkn Aerospace, SE G. PALAIA, University Of Pisa, IT P. ALEXANDRE, SABCA, BE
18:50 END OF DAY1
TRANSFER TO BORDEAUX COUNTY HALL (TRAM) 20:00 - 22:30 COCKTAIL PARTY BORDEAUX COUNTY HALL
Wednesday 26th February 2020
09:00 - 10:00 PLENARY SESSION 3 Chair : Rafael Bureo Dacal, ESA KEYNOTE SPEECH 3: Common aeronautics-space technologies, Pascale Ehrenfreund, Chair of the Executive Board, DLR
KEYNOTE SPEECH 4: Space Electric propulsion, José Gonzalez del Amo, Head of the Electrical Propulsion Section, ESA
10:00-10:30 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 28 : Alternative Fuels Session 29 : Assessment of ACARE Goals Session 30 : Advanced Design Methods for Novel Session 31 : Low Noise Session 32 : Manufacturing & processes Session 33 : Electric Powered Aircraft: Rationale, Session 34 : REMAP Workshop Session 35: Structures, Thermal and Mechanisms II Session 36: Space Propulsion IV Moderation: Delia Dimitriu (MMU) Chair M. Kyriakopoulos (EC) Aircraft Concepts Design Methods Chair: S. Shroff (CS) Platform, Propulsion and Wing Design Chair: O. Pin (ESA) Chair: J. Gonzalez del Amo (ESA) Chair: J-F. Brouckaert (CS) Chair: D. Gely (ONERA) Chair: F. Boudjemaa (Safran)
10:30-10:50 533 405 610 290 583 335 739 166 Alternative fuels as a path to lower emission aviation Results and Exploitation of the Project PARE Framework development for robust design of novel Progress in aeroengine noise reduction through Aerothermal characterization of a compact heat The whole truth about electric-powered flight for civil Reduced order models and machine learning The impact of the SPT-140D parameters and lifetime A. SHUSTOV, TsAGI, RU (Perspectives for Aeronautical Research in Europe) aircraft concepts advances in diagnostics and computational methods exchanger element by additive manufacturing transportation: From Breguet to operational aspects algorithms to develop predictive thermal tools for characteristics change on its thermal mode L. BRAGA CAMPOS, Ist, Lisbon University, PT M. SAPORITO, University Of Southampton /ONERA C. RICHTER, Rolls-Royce Deutschland, DE D. LABOUREUR, Von Karman Institute,BE I. STAACK, Linköping University, SE spacecraft simulations L. KROCHAK, Edb Fakel, RU Toulouse, FR C. SEMLER, Maya Htt, CA
10:50-11:10 279 399 174 384 81 505 029 302 Study of NH3 as a CO2-free fuel for the propulsion of Analysis and Forecast of Change of Fuel Efficiency Recent advances in establishing a common language Toward Optimal Design of Contra-Rotating Alternative materials and process for structural parts Conceptual design and optimization of a general Innovative concept for additive manufacturing of Preliminary Analysis of High Performance Low-Cost commercial airplanes Indicator of Passenger Airplanes for aircraft design with CPACS Propulsion System - Practical Acoustic Analysis manufacturing aviation aircraft with fuel cells and hydrogen as compliant mechanisms Blended Monopropellants Based on High Test N. CAMARA AGUIAR, Altran, ES V. LOGINOV, Ivchenko-Progress Se, UA M. ALDER, DLR, DE O. GUR, Iai - Israel Aerospace Industry, IL J. J. EGURROLA, Leartiker S. Coop., ES propulsion system L. KIENER, Csem, CH Peroxide S. NICOLAY, Tu Braunschweig, DE E. FONDA-MARSLAND, University Of Southampton, GB
11:10-11:30 298 402 260 529 377 043 579 272 Enabling Cryogenic Hydrogen-Based CO2-free air Attraction of women and young talent to Aeronautics An automated approach for the aerodynamic design CFD-based prediction of wall-pressure spectra under Numerical continuity as a tool for process Hydrogen Drone Research Aircraft Numerical Ballistic Limit Equation for explosion of Hydrocarbon Augmented Water Electrolysis transport (PARE Project) of close-coupled propulsion/airframe configurations a turbulent boundary layer with adverse pressure development and improvement for manufacturing R. VAN BENTHEM, Royal Netherlands, Aerospace Hydrazine-filled tanks Propulsion D. NALIANDA, Cranfield University, GB Q. COSTA, Inova+, PT J. MATESANZ GARCIA, Cranfield University, GB gradient future SX high pressure turbine blades Centre, NL C. PUILLET, Cnes, FR A. HERBERTZ, ESA, NL G. GRASSO, Ecole Centrale De Lyon, FR J, AGUILAR, Safran, FR
11:30-11:50 451 558 032 508 349 190 585 083 Multifunctional fuel cell for aeronautics PARE analysis of ACARE Flightpath 2050 Preliminary Aircraft Design within a Multidisciplinary Numerical simulation of the broadband noise of a Automated Cabin and Cargo Lining and Hat Rack On the Design of an Electric-Powered Micro-Feeder The Deployment System of the Flexible Solar Array Hydro-thermodynamic behavior of a hydraulic REMAP WS S. MATHONNIERE, Ametra, FR environmental impact goals and Multi-fidelity Design Environment counter-rotative open rotor configuration using Installation for the Aircraft Factory of Tomorrow Aircraft Technology GoSolAr restriction in liquid nitrogen in steady-state and fluid- see detailed programme at the end of the file O. ZAPOROZHETS, National Aviation University, UA S. WÖHLER, DLR, DE phase-lagged conditions - Part1: initial validation on L. BRIESKORN, Fraunhofer Ifam, DE A. ROLANDO, Politecnico Di Milano, IT C. HÜHNE, DLR, DE hammer conditions a single rotor case L. PEVERONI, Von Karman Institute, BE M. FIORE, Cerfacs, FR
11:50-12:10 670 559 572 687 46 40 371 237 Modeling of new fuels emergence impact on the air Aircraft emissions and European ACARE goals : Aerodynamic design procedures and tools for box- Acoustic bass field effect on an array of premixed DSLM processing of optimized Active Flow Control All Electric Intercity-Aircraft Design Based on Fuel Spaceborne Unfurlable Reflector Antenna Design of a 1-N monopropellant thruster for testing transportation market synthesis of FORUM-AE conclusions wing transport aircraft flames Actuators for UHBR engine aircrafts Cell Energy System. Technologies In Europe: Current Status and Future of new Hydrogen Peroxide decomposition E. VARYUKHINA, Nrczh Named After Zhukovsky, RU O. PENANHOAT, Safran, FR K. ABU SALEM, Università Di Pisa, IT A. RANGBULLA, University Of Toronto, CA A. M. MANCISIDOR, Lortek S. Coop, ES G. ROMEO, Politecnico Di Torino, IT Outlook technologies G. RODRIGUES, Esa, NL T. FRANKEN, Delft University Of Technology, NL
12:10-12:30 249 157 626 742 636 250 007 263 How to promote the use of e-fuels fuels in aviation? - Overview and Challenges of EU Aviation Noise Aerodynamic optimization of the fuselage-pushing Assessment of Shielding Effect Efficiency for BWB Development of a REACh compliant multifunctional Position dependency of the Aerodynamic Multi-DOF microvibration isolator with contactless On P80 SRM QSS Pressure Oscillation Dispersions Recommendable policy measures for a carbon Reduction Research propeller configuration with UHBR coating for rain erosion, corrosion resistance and Interactions between Wingtip-Mounted Propellers actuators M. GROSSI, Sapienza University of Rome, IT friendly air transport system D. COLLIN, Safran, FR V. GUBSKIY, TsAGI, RU V. KOPIEV, TsAGI, RU aesthetical aerospace requirements of aluminum and the Wing-Vortex-System trough numerical L. VICENTE, Université Libre De Bruxelles, BE J. SCHEELHAASE, DLR, DE large parts by plasma electrolytic oxidation Simulation J. ESCOBAR, Irt Saint Exupery, FR M. SCHOLLENBERGER, University Of Stuttgart, DE
12:30 - 13:40 LUNCH 13:40 - 15:00
ROUND TABLE 1: From research to flight: bridging the death valley Moderator: Philippe Landiech, Head of Spacecraft Architecture, Validation & Integration Department, CNES Participants: Philippe Beaumier, Aeronautics Director, ONERA Sergey Chernyshev, IFAR President, Chief Scientist TsAGI Frederic Teston, Head of the Systems, ESA Jean-François Brouckaert , Chief Scientist, Clean Sky Hervé Gilibert, CTO Ariane Group
ANERS AERONAUTICS SPACE Session 37 : Green Operations Session 38 : Flow Control Session 39 : New Aircraft Configurations Session 31 Cont'ed : Low Noise Session 40 : Numerical methods, CFD Session 33 Cont'ed : Electric Powered Aircraft: Session 41: Clean Space, Space Debris III Session 42 : Spacecraft Design Session 43 : Testing II Moderation: Sigrun Matthes (DLR) & John-Paul Chair: F. Collier (NASA) Chair: J-F. Brouckaert (CS) Design Methods Chair: V. Selmin (CS) Rationale, Platform, Propulsion and Wing Design Chair: R. Bureo (ESA) Chair: N. Viola (POLITO) Chair: C. Bonnal (CNES) Clarke (UTC & Georgia Tech) Chair: D. Gely (ONERA) Chair: F. Boudjemaa (Safran)
15:00-15:20 130 004 126 500 019 200 133 014 316 4D Trajectory Optimization with Atmospheric Oscillatory Suction and Pulsed Blowing Actuator Wing twist optimization for the passenger aircraft Overview of ONERA contribution to the Computing flow sensitivities in a high-order CFD Design and Development of Thrust Vectored Vertical Evaluation of Ballistic Limit Equations for standard Exomars: Lightweight Structural Design for Extreme Inovative Design and Technologies for Developing Forecast Parameters B. MIZRAHI, Tel Aviv University, IL with hybrid propulsion aeroacoustics design and assessment of the high- code using automatic differentiation Take-Off and Landing (VTOL) Electric Powered Multi Layers Insulations with stand-off to units Exoplanet Environments Wide Range Thermal Facilities for JUICE Large A. VITALI, Politecnico Di Torino, IT T. GOETZENDORF-GRABOWSKI, Warsaw University of speed helicopter demonstrator RACER J. CARDESA, Institut De Mécanique Des Fluides De Autonomous Unmanned Aerial Vehicle C. PUILLET, Cnes, FR D. CHRISTOU, Airbus, GB Appendage and Subsystems Technology, PL A. LE PAPE, ONERA, FR Toulouse (Imft), FR W. MIRZA WASIF SAEED, Nazeer Hussain University, D. IFRIM, Comoti, RO PK
15:20-15:40 493 340 267 459 187 598 718 660 289 Permanent Resume Trajectory: an innovative FMS An Experimental Investigation of a 3D Morphing Flap Conceptual Design Studies of Unconventional CAbin NOise from Boundary Layer Excitation - Evaluation of turbulence models for the prediction of Method for analysis of flight characteristics of eVTOL Evaluating the shielding capability of a satellite Multi- Design and Development of DALBIT-1: Earth-based Combustion stability characteristics of a sub-scale functionality for greener and seamless operations Deflection Configurations CANOBLE Cleansky2 project vortex interaction over a fighter aircraft scaled model Layer Insulation against space debris impact lander testbed LOX/LNG rocket thrust chamber J. BOYER, Thales Avs, FR F. MADI, University Of The West Of England, GB M. IWANIZKI, DLR, DE R. LENEVEU, Vibratec, FR E. GUILMINEAU, Cnrs - Ecole Centrale De Nantes, FR T. KOSEL, Faculty Of Mechanical Engineering, University H. ABDULHAMID, Thiot Ingenierie, FR C. SUKMIN, Kaist, KR J. HARDI, DLR, DE Of Ljubljana, SI
Session 44: Acoustic Liners Chair: J. Mardjono (Safran)
15:40-16:00 491 191 265 30 225 375 105 124 238 FlytOptim – crew assistance for greener and safer In plane wavy streamwise wall forcing for turbulent Conceptual Design Studies of Boundary Layer Clean Sky’s IDEAS project: Innovative DEsign of The Impact of Compressibility on Kinetic Energy Investigation into the viability of integrated regional Results, opportunities and limitations of Turbine blade design methodology for a rocket Vibroacoustic predictions and test campaign for the flights skin friction drag reduction Ingestion Engine Integration Concepts acoustic liners for Air conditioning Systems Evolution within Framework of Large Eddy air transport based on all-electric aircraft implementing LCA and ecodesign in a space context engine turbopump exomars structural and thermal model F. PRENOT, Thales Avs, FR N. BENARD, Cnrs Pprime, FR M. MEHEUT, ONERA, FR E. PIOT, ONERA, FR Simulation R. BARRIER, Cranfield University, FR – Experiences from the Greensat study C. DOBROMIRESCU, COMOTI, RO P. ROSARIO, Airbus, GB Z. LI, Cranfield University, GB A. VERCALSTEREN, Vito, BE
16:00-16:20 412 264 212 150 466 551 028 242 Assessment of takeoff automation for operational Development of high authority synthetic jet actuators Integration of an Over-Wing Mounted Engine on a Development of Resin-based Lightweight Acoustic Epsilon: An Open Source Tool for Exergy-Based Aeroelastic Analysis of Electric Aircraft Wings Green Solutions for Space Propulsion A new single-wheel test bed for fast-moving noise reduction for aerospace applications mid-range aircraft Liner in aFJR project Aerodynamic Analysis Subjected to Propeller Thrust and Angular U. GOTZIG, ArianeGroup GmbH, DE planetary robots B. BASTOS ZANETTI, Embraer, BR B,GUNGORDU, University Of Nottingham, GB P. WEGENER, DLR, DE R. KAGAYA, Ihi Corporation, JP M. A. AGUIRRE, ISAE, FR Momentum K. KAZUKI NAKAGOSHI, Tohoku University, JP S. FAZELZADEH, University Of Huddersfield, GB
16:20-16:50 COFFEE BREAK Session 37 Cont'ed : Green Operations Session 38 Cont'ed : Flow Control Session 39 Cont'ed: New Aircraft Configurations Session 44 Cont'ed: Acoustic Liners Session 40 Cont'ed: Numerical methods, CFD Session 45 : CS2 Active Flow Control Session 46: Materials and Advanced Manufacturing Session 47 :Testing III Session 48 : Space Guidance, Navigation and Control Moderation: Sigrun Matthes (DLR) & John-Paul Chair: F. Collier (NASA) Chair: J-F. Brouckaert (CS) Chair: J. Mardjono (Safran): Chair: V. Selmin (CS) Chair: B. Stefes (Airbus) for Space Application II Chair: K. Pfaab (CNES) GNC Clarke (UTC & Georgia Tech) Chair: C. Huehne (DLR) Chair: G. Ortega (ESA)
16:50-17:10 707 241 164 681 404 45 569 042 675 The Impact of Descent Thrust on Fuel Consumption Active panel flutter control of composite plates with Preliminary design of a blended wing body airliner Characterization of sonic crystal acoustic absorbers A Better Assessment of the Recoverable Energy Miniature airworthy fiber optic pressure sensor for Regulatory and commercial obsolescence risks of European Research and Technology Test Facility An Improved Extended Kalman Filter for Nonlinear and CO2 Emission piezoelectric stiffener actuators for improved fuel efficiency produced by fugitive ink manufacturing process Behind a Body by the Exergy Method measuring static pressure and acoustics materials and processes P8.3 for full Cycle Investigations of Subscale Rocket State Estimation H. AKSOY, Eskişehir Technical University, TR Y. KAIHUA, Beijing Institute Of Mechanical And Electrical P.C.BERRI, Politecnico Di Torino, IT R. E. FOTSING, Polytechnique Montréal, CA M. A. AGUIRRE, Safran, FR S. KIENITZ, Fos4x, DE P. HEISKANEN, ESA, NL Engines M. DE FREITAS COELHO,University Of Beira Interior, PT Engineering, CN D. LINDNER, DLR, DE
Session 49 : Ecodesign and Green Life Cycle Chair: L. Paletti (NLR)
17:10-17:30 561 644 499 355 125 376 354 023 635 A multi-objective route allocation model taking GLOWOPT – A new approach towards global- Exploration and Optimization of a Blended Wing- On the Using of Vacuum Technology for Noise Numerical study of NASA Rotor 67 under running CFD ans Wind Tunnel Tests for Local Active Flow Failure criteria for CFRP composites in the cryogenic Role of subscale tests in engines development Proximity operations trajectory design in the relative aircraft sequence and separation into account warming-optimized aircraft design Body concept featuring distributed electric Reduction at Aircraft conditions on an unstructured hybrid mesh Control at the Wing-Pylon-Nacelle Junction regime programs orbital elements’ perspective V. HO-HUU, Delft University Of Technology, NL F. LINKE, DLR, DE propulsion C. SANDU, Incdt-Comoti, RO H. ISHIKAWA, JP V. CIOBACA, DLR, DE J. HOHE, Fraunhofer IWM, DE D. SUSLOV, DLR,DE G. GAIAS, Politecnico Di Milano, IT A. SGUEGLIA, Isae-Supaero & ONERA, FR
17:30-17:50 35 151 221 553 437 454 038 015 621 Environmental Friendly And Affordable Small Aircraft Assessing the Effect of Hybrid-Electric Power-Trains Aeroelastic Optimization of a Blended Wing Body SALUTE Project : Main objectives and primary results Characteristics and Generation Mechanism of Active flow control of Wing-Engine-Slat cut-out flow Optimization of Selective Laser Melting Process ETID NE hot-fire test campaign Station-keeping for halo orbits using a solar sail with Transport To Improve European Network on Acoustic and Chemical Pollution Aircraft K. BILLON, ECL, FR Broadband Noise from Compressor Cascade separation using suction and pulsed blowing Parameters for High Density IN625 Parts L. BROX, GKN Aerospace, SE one-degree-of-freedom electric propulsion D. G. ROMANO, Piaggio Aero Industries S.P.A., IT C. RIBOLDI, Politecnico Di Milano, IT J. MAS COLOMER, Isae-Supaéro, FR Y. MITSUSUE, University Of Tokyo, JP S. MONAT, Tel Aviv University, IL G. MATACHE, COMOTI, RO J. BIGGS, Politecnico di Milano, IT
17:50-18:10 53 104 504 560 549 122 033 047 467 New Mobility Concepts: Optimisation of Flight HALE multidisciplinary design optimization with Re-Thinking the Long-Haul Air Transport Segment D02/R02 Development and Assessment of a LEONAR Compressible Navier-Stokes analysis of eVTOL Wall Shear Stress Measurements of Magnitude and Increasing the acceptance rates of additively Guidelines For Cryogenic Adhesive Testing Resilient Redundant Spacecraft GN&C's Propulsion Movements in Europe focus on Eco-Material selection F. TROELTSCH, Bauhaus Luftfahrt E.V., DE Acoustic Liner Design for Landing Systems Noise propulsion using a low-speed preconditioned Direction in non-steady flows manufactured components using Image Based Finite M. LEITWEIN, University Of Applied Sciences, DE System Fault Detection and Diagnostics F. THIESSEN, Tu Chemnitz, DE E. DURIEZ, Isae-Supaero, FR Minimization multigrid iteration compared to experimental results M. STAATS, Tu Berlin, DE Element Modelling (IBFEM) K. KAWATSU, Jaxa, JP A. GHOUALI, ONERA, FR T. KOSEL, Faculty Of Mechanical Engineering, University T. ETHERIDGE, Airbus, GB Of Ljubljana, SI
18:10-18:30 188 51 373 325 441 452 034 705 Optimal Sizing and Operations of a Battery Sustainability Driven Product Development in Studies on aerodynamic layouts formation of eco- Experimental study of a very thin acoustic Simulation Tool For Environment Friendly Aircraft Numerical Study of Active Flow Separation Control A novel semi-automated manufacturing process for X- Attitude Dynamics and Control of a Large Flexible Recharging Infrastructure for a Regional Airport Aviation friendly transport aircraft metasurface Cargo Fire Protection System Evaluation for UHBR Engine Integration on Generic Wing in High- ray and γ-ray imaging grids Space Structure by Means of a Minimum Complexity F. SALUCCI, Politecnico Di Milano, IT A. KÖTTER, Altran Deutschland Sas, DE E. PIGUSOV, Central Aerohydrodynamic Institute,RU superabsorber for future aircraft V. NORREFELDT, Fraunhofer Ibp, DE Lift Configuration N. GRADWOHL, University Of Applied Sciences Model M. DEACONU, Incdt-Comoti, RO A. PRACHAR, Vzlu - Czech Aerospace Research Centre, Northwestern Switzerland, CH G. AVANZINI, Università Del Salento, IT CZ
18:30-18:50 189 91 257 696 214 Reducing Greenhouse Emissions from Air Transport Way to greener bizjets Noise control of the centrifugal compressor by using Development of fluid–structure interaction method Array of synthetic jets for large passenger aircraft (189) J. LE GALL, Dassault Aviation, FR open-cell metal foams for flutter analysis of laminar wing M. LIPOWSKI, Fraunhofer-Institut Für Elektronische R. SPENCER, Nangia Consulting, GB X. CHEN, Xi'an Jiaotong University, CN S. KUZMINA, TsAGI, RU Nanosysteme Enas, DE
18:50 END OF DAY2
TRANSFER TO DINNER VENUE (TRAM)
20:00 GALA DINNER (PALAIS DE LA BOURSE)
END OF DAY2
TRANSFER TO DINNER VENUE (TRAM)
GALA DINNER (PALAIS DE LA BOURSE) 23:00
Thursday 27th February 2020 09:00 - 10:00 PLENARY SESSION 4 Chair: Valérie Guénon, Safran KEYNOTE SPEECH 5: Green bizjet technological developments within aeronautical research programmes , Bruno Stoufflet, CTO Dassault Aviation and Vice-Chairman of CORAC
KEYNOTE SPEECH 6: The Route to Sustainable Aviation, Paul Stein, CTO Rolls-Royce
10:00 - 10:30 COFFEE BREAK ANERS Aeronautics Space Auditorium A R01 (G1+G2) R02 (D1+D2) R03 (F1) R04 (E1) R05 (E2) R06 (F2) Session 50 : Emissions Session 51 : High Speed Transport Session 52 : Evaluation of New Concepts Session 53 : Testing, Design methods & concepts I Session 54 : Materials Modelling, Analysis and Session 55 : Green and safe systems & operations II Session 56 : Space Structures, Thermal and Moderation: Paul Madden (RR) & Olivier Penanhoat & Environment Chair: C. Hermans (DNW) Chair: C. Hillenherms (DLR) Testing Chair: M. Bourgois (Eurocontrol) Mechanisms III (Safran) Chair: S. Chernyshev (TsAGI) Chair: S. Shroff (CS) Chair: P. Corberand (Airbus Defence And Space)
10:30-10:50 653 620 581 138 699 202 162 Impacts of cloud layers overlap on contrail- A Method for Supersonic Commercial Market An analytical approach to determine the impact force Rapid Wind Tunnel Testing & Advanced Finite element analysis of composite double-swept Optimal Definition of a Short-Haul Air Transportation Fiber Bragg Gratings for prognostics in space attributable radiative forcing Estimation and Environmental Impact Evaluation of small unmanned aerial vehicle collisions with rigid Instrumentation – Future Testing Pillars helicopter blades using node dependent kinematics Network for Door-to-Door Mobility applications: a thermo-mechanical characterization I. SANZ-MORÈRE, MIT, US C. WEIT, Georgia Tech / Cnrs, US and elastic targets P. WHITE, Airbus Operations Ltd., GB M. FILIPPI, Politecnico Di Torino, IT L. TRAINELLI, Politecnico Di Milano, IT of minimally invasive sensing techniques F. FRANKE, Technische Hochschule Ingolstadt, DE P. C. BERRI, Politecnico Di Torino, IT
10:50-11:10 70 496 591 239 562 010 129 The contribution of carbon dioxide emissions from Key technologies for new generation SST HUMS, enabling technology reconciling ecodesign Common Numerical Methods & Common Bayesian reconstruction of goal orientated error Experimental setup to measure and analyze ice EC H2020 Large Deployable European Antenna (LEA) the aviation sector to future climate change A. KAZHAN, TsAGI, RU and global value proposition in a Circular Economy? Experimental Means for the Demonstrators of the fields in large aerospace finite element models adhesion on Air Cycle Machine turbine exit pipe M. KOSMALSKI, Hps Gmbh, DE E. TERRENOIRE, ONERA, FR K. LE BLEVENNEC, VITO, BE Large Passenger Aircraft Platform M. BONNEY, University Of Nottingham, UK surface W. KRUEGER, DLR, DE A. VINCENT, Cranfield University, UK
11:10-11:30 215 652 016 013 108 251 063 Mitigation potential of climate-optimized routing: Global emissions estimation for commercial An overview of the current and future aircraft Aircraft Engines Test Facilities Design Optimization Dry Sliding Behavior and Particulate Emissions of a Thermal-Dynamic Investigation of Advanced System Closing force evaluation of a sample return capsule concept study for Europe supersonic fleets under different design and environmental control system and its air filtration for Flight Increased Safety and Environment Impact SiC-Graphite Composite Material for Braking Systems Control Strategies for Decentralized Electro-Hydraulic for a Phobos Sample Return mission S. MATTHES,DLR, DE regulatory scenarios system Reduction P. JAYASHREE, University of Trento, IT Power Generation in More Electric Aircraft R. MIHALACHE, Romanian Research and Development I. SANZ-MORÈRE, MIT, US E. ZAVAGLIO, UTRC, IE V. SILIVESTRU, COMOTI Romanian Research and N. TROCHELMANN, Hamburg University Of Technology, Institute for Gas Turbines COMOTI, RO Development Institute for Gas Turbines, RO DE
11:30-11:50 134 693 107 481 226 458 252 Aviation's air pollution impacts in a changing world: STRATOFLY MR3: towards a complete Development of Fault Tolerant Electro-Mechanical Development of a Multifunctional Fuselage Simulation of the impact behavior of various Passive anti-icing system using pass-through Wall Roughness Modeling in Rocket Combustion effects of changing background atmospheric decarbonization of long-haul routes Actuation System for Ailerons of Regional Aircraft Demonstrator materials evaporator capillary pumped loop Chambers composition R. FUSARO, Politecnico Di Torino, IT T. RIPEL, Honeywell, CZ S. VELDMAN, Fokker, NL Y. TOSO, DLR, DE R. RIOBOO, Euro Heat Pipes, BE O. RAFFAELE, Technische Universitaet Muenchen, DE I. DEDOUSSI, TU Delft, NL
11:50-12:10 584 690 689 576 734 056 235 Safran ultrafine particles campaigns in 2019 H2020 STRATOFLY Project: technical and Image-Based Path Following Control of an New Concepts of Environmentally Friendly High-Lift Optical fibre Bragg grating sensors for BVID Ground Loads Time Monitoring System Structural vibration control with passive isolation P. DUCHAINE, Safran, FR operational challenges of hypersonic flight Unmanned Quadrotor Devices and Their Application in a Small-Aircraft- detection on composite sub-components E. GOMEZ, Airbus, ES system for propulsion equipment N. VIOLA, Politecnico Di Torino, IT H. HITOMU SAIKI, National Research Institute Of Fire Transport Area S. GOOSSENS, Vrije Universiteit Brussel, BE P. ROSARIO, Airbus, GB And Disaster, JP W. STALEWSKI, IoA, PL
12:10-12:30 158 745 127 Airport in a Decarbonising Transport System, the Design of sonic boom simulators for low boom day Hybrid Sheet Moulding Compound With Carbon Impact of Convergence in Disruptive Technologies and night, noise and vibration perception studies Prepregs and Services F. COULOUVRAT, CNRS, FR J. SILVA, Inegi, PT D. DIMITRIU, Manchester Metropolitan University, GB
12:30-13:40 LUNCH 13:40 - 14:40 ROUND TABLE 2: Electric/hybrid Propulsion Moderator: Rolf Henke, DLR Executive Board Member for Aeronautics Research Participants: Stéphane Cueille, CTO Safran, Jean Brice Dumont, Executive Vice President Engineering, Airbus Mike Benzakein, former CTO GE, Assistant Vice President for Aerospace and Aviation Research Univ. Ohio State
ANERS Aeronautics Space Session 50 Cont'ed : Emissions Session 51 Cont'ed : High Speed Transport Session 57 : CLEAN SKY Technology Evaluator Session 58 : Propulsion Session 54 Cont'ed : Materials Modelling, Analysis Session 59 : Autonomous Aircraft Operations Session 60 : Mission Design and Space Systems I Moderation: Paul Madden (RR) & Olivier Penanhoat & Environment Chair: J-F. Brouckaert (CS) Chair: V. Guénon (Safran) and Testing Chair: T. Melin (FOI) Chair: P. Landiech (CNES) (Safran) Chair: S. Lemaire (Dassault) Chair: S. Shroff (CS)
14:40-15:00 232 495 155 261 747 638 069 Case study on the environmental impact and The influence of the overpressure signature shape Clean Sky 2 „Technology Evaluator“ Methodology assessment for the design and analysis Innovative manufacturing and numerical modelling 4D Flight Trajectory Optimization by Modified CNES Balloon systems and activities efficiency of travel on the sonic boom loudness N. FLUETHMANN, DLR, DE of aero-engine short intakes of thermoplastic and thermoset composite structures Dynamic Programming Approach V. DUBOURG, Cnes, FR E. OTERO, KTH, SE A. KAZHAN, TsAGI, RU L. BOSCAGLI, Cranfield University, GB for SHM aerospace application A. KAWSER, University Of Beira Interior, PT M. MORA-MENDIAS, FIDAMC, ES
Session 61 : Structures Design Chair: P. Schmollgruber (ONERA)
15:00-15:20 571 555 089 605 403 720 103 Marginal Climate and Air Quality Costs of Aviation Supersonic aircraft compliance with noise Environmental Impacts of Clean Sky 2 Technologies Clean Sky 2 Large Passenger Aircrafts - Techno Architecture-based conceptual design for mechanical Optimized Sampling for Environmental Monitoring Venus sample return mission revisited Emissions requirements to LTO performances and airport noise for Next Large Passenger Aircraft Bricks for future engines systems applied to landing gear with Airborne Sensors D. VALENTIAN, Itg, FR C. GROBLER, MIT, US exposure/impact assessment and management P. ARBEZ, Airbus Sas, FR C. DIETTE, Safran Aicraft Engines, FR E. ALLEGAERT, Siemens, BE G. AVANZINI, Universirà del Salento, IT O. ZAPOROZHETS, National Aviation University, UA
15:20-15:40 RT2 Emissions Session Concluding Round Table 358 099 482 445 594 723 On the Possibility to Reduce the Intensity of Shock Clean Sky 2 TE – Environmental impact assessment Future Aircraft Propulsion-A Preliminary Overview of Experimental and numerical study of the composite Determination of acoustic characteristics of Dynamic Motion of a Descent Vehicle during the Paul Madden (RR) & Olivier Penanhoat (Safran) Waves Using Meshes with Application to Supersonic at airport level Difficult Choices wing structure embedding solar cells Autonomous Aircrafts for environment protection Landing Stage and Hypersonic Vehicles M. VAN EENIGE, NLR, NL F. KIRKLAND, University Of Nottingham, GB Q. ROUXEL, Gem – Institut De Recherche En Génie Civil and collision avoidance in flight restricted zones M. HERMOSILLA, School Of Aeronautical And Space C. SANDU, COMOTI, RO Et Mécanique, FR V. MAKARENKO, National Aviation University, UA Engineering, Technical University Of Madrid, ES
Session 62 : ANERS Session 63 : Mission Design and Space Systems II Final Session Chair: P. Landiech (CNES)
RT3 Environmental Interdependencies: 228 295 337 008 141 401 D. Mavris (Georgia Tech) Noise Reduction of Supersonic Civil Aeroplane at Design Evaluation and Performance Assessment of Multi-fidelity assessment of exhaust systems for Passenger aircraft composite centre wing box Environmental Benefits of Cooperative Obstacle Future-Oriented Research Platform For Orbital D. Zingg (UTIAS) Takeoff And Landing Using Programmed Engine Fast Rotorcraft Concepts in the 2050 timeframe complete engine-aiframe configurations structure optimization Avoidance for Unmanned Aerial Vehicles using Cryogenic Storage Technologies (FROST) 15:40-16:00 E. Kors (Safran) Thrust Control D. NALIANDA, Cranfield University, GB J. HUESO REBASSA , Cranfield University, GB M. KOWALSKI, Warsaw University Of Technology, PL Artificial Potential Field T. E. BRUNS, DLR, DE M. Viinikainen (FINAVIA) I. KHALETSKII, Central Institute Of Aviation Motors, RU D. P. MIREA, University of Bristol, UK A. Garcia Sainz (ARC) B. Ollenforst (NLR)
Moderation: Delia Dimitriu (MMU) & Fay Collier (NASA) 16:00-16:20 577 421 492 167 334 629 Design Optimization and Dynamic Characterization of European TRANSCEND for novel aircraft propulsion VHBR Propulsion Technology – Smart Integration of Investigation of Load Collectives on Transport GPAHRS – navigation enabler for more autonomous Modern Techniques and Technologies for Space a Tailless High Speed Aircraft Configuration and alternative fuels roadmaps towards 2050 Demonstrators and Techno-Bricks Aircraft Using Continuous Turbulence for Fatigue aircraft Flight Vehicle Engineering C. NAE, Incas, RO J. KOS, NLR, NL V. MELBOURNE, Rolls-Royce Plc, GB Analysis Purposes G. BOURELY, Honyewell International, CZ G. ORTEGA, European Space Agency, NL V. HANDOJO, DLR, DE
16:20-16:50 COFFEE BREAK Session 62 Cont'ed : ANERS Session 64 : Urban air mobility and its impact on the Session 65 : Testing, Design methods & concepts II Session 58 Cont'ed : Propulsion Session 61 Cont'ed : Structures Design Session 66 : Satellite Communications & Operations, Session 63 cont'd : Mission Design and Space Final Session environment Chair: C. Hillenherms (DLR) Chair: G. Way (Rolls Royce) Chair: P. Schmollgruber (ONERA) Software and Robotics Systems II Chair: J.-L. Strèque (Thalès) Chair: R. Bureo (ESA) Chair: P. Landiech (CNES)
16:50-17:10 RT3 Environmental Interdependencies: 053 292 479 048 060 550 D. Mavris (Georgia Tech) New Mobility Concepts: Optimisation of Flight Wall-modelled LES (WMLES) of flow conditioners Testing a future UHBR low-speed fan Failure modes analyses and impact on aeroelastic Design, manufacturing and testing of an antenna The Impact of Superconductor-Based Power System D. Zingg (UTIAS) Movements in Europe E. HODZIC, Queen's University Belfast Uk V. MELBOURNE, Rolls-Royce Plc., GB stability of a regional aircraft equipped with reflector for deep space missions Architectures On Payload Mass Fraction E. Kors (Safran) F. THIESSEN, Tu Chemnitz, DE morphing winglets D. MIHAI, COMOTI, RO Optimisation M. Viinikainen (FINAVIA) I. DIMINO, CIRA, IT M. COLLIER-WRIGHT, Neutron Star Systems, DE A. Garcia Sainz (ARC) B. Ollenforst (NLR)
360 338 671 139 524 17:10-17:30 Moderation: Delia Dimitriu (MMU) & Fay Collier A Methodology and first Results to assess the Comparison of two different flow diverters for Parametric Study of a Solid Propellant Slotted Grain Impact Resistant and Low-Weight Composite AI Enhanced Multi Media System Architecture for (NASA) potential of Urban Air Mobility concepts inverted inlet O. YAQUOB, Military Technical College, EG Solution for Aircraft Fuselage Human Habitation in Space Mission V. GOLLNICK, Hamburg University Of Technology, DE T. REN, Beijing Electro-Mechanical Engineering Institute, R. RICARDO JORGE BRAGA ROCHA, Inegi,PT H. KESUMA, Aes – Aircraft Elektro/Elektronik System CN Gmbh, DE
17:30-17:50 Symposium Closing Speech 392 695 052 627 Future Sky Urban Air Mobility: An Outlook on the Supersonic Flow Analysis on Different Multi-Row Effects of Material and Geometrical Parameters on Ice Digging Robot with Navigation J. HILEMAN (FAA) New Thematic Programme within the EREA Joint Inlet Devices the Design of a Trailing Edge Twist and Camber P. CATALIN, Incas, RO Research Initiative G. SINGH, Amity University Uttar Pradesh, IN Morphing Surface C. ESCHMANN, DLR, DE Y. ZAHOOR, Tu Delft, NL
Moderation: Dominique Collin (Safran)
17:50-18:10 668 580 Applications of a novel Semi-Active Piezoelectric Emergence of Airware® 2050 for Space applications Tuned Mass Damper for Vibrations Mitigation in M. NIEDZINSKI, Constellium, US Aircraft Structures N. CHRYSOCHOIDIS, Patras University, GR
18:10 - 19:00 PLENARY 5 - CLOSING: Chair Z. Goraj, TU Warsaw, CEAS President KEYNOT SPEECH 7: Clean Aviation in Horizon Europe – status and views from the European Commission, Hervé Martin, Head of Unit "Low Emission Future Industries" Directorate-General for Research and Innovation, Clean Planet, European Commission Best paper Awards ceremony
19:00 - 21:00 WINE TASTING CONGRESS CENTER
END OF THE CONFERENCE
POSTERS: From 25th to 27th February 2020 the posters will be displayed in the exhibition area
Friday 28th February 2020
TECHNICAL VISITS (from 9h00 to 13h00) - Arianegroup Issac premises - Dassault Aviation - Thales
WINE TOUR (from 10h00 to 17h00, additional cost for the participants)
ReMAP Workshop