Chaired by :

Mr. Christophe Bonnal, EUCASS, France

General instructions for poster authors

  • The title of your poster must appear at the top in 25 mm-high capital bold letters.
    Make sure that the authors and their corresponding organizations are clearly visible.
  • Your Poster shall be format A0 portrait (vertical) = 0.84m x 1.19m.
  • You shall come with your poster ready to attach; there are no ways to print your poster at the congress center.
  • Pins to attach your poster to the support are provided by the congress center.
  • We ask you to attach your poster upon arrival at the Congress Center, Monday morning, and leave them until Thursday afternoon.
  • We have planned 2 Poster Sessions on Tuesday and on Wednesday, from 15:30 to 16:30, with no other session in parallel, where we ask you to be close to your poster to discuss with the delegates, explain, answer questions, network.
  • The display will be done on support panels as shown below:

Note that the panels will each have a number at the top left corner, set from 1 to 70. This number corresponds to the session number of your poster that you can find in the far right column in the table below.
keep that number in mind, you will then be able to pin you poster on the correct panel.

You can view the floor plan with the poster panels here.

List of Posters

You can search and sort the table to your convenience by using the SEARCH area above the table, and the pagination system at the bottom.

Deyou Wang; Ge Jin; Ruyao Wang; Shipeng LiFlow separation characteristics of supersonic nozzles in water environmentBeijing Institute of TechnologyUnderwater jet propulsion; Supersonic nozzles; Flow separation; Water environment; Unsteady characteristicsAEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies1
StoliaroffAriane 6 IMA Separation TestArianegroupSeparation; test; Ariane 6AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies2
Benjamin Khiar; Fabien Tholin; François Pechereau; Denis PackanModelling of MHD flow control for atmospheric re-entryONERAMHD; re-entry; flow control; hypersonic; magnetic fieldAEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies3
Yann BLAIRON; Olivier MONTAGNIER; Annie LEROYDynamic stall models for post flutter analysis of an aeroelastic wing sectionÉcole de l'Air et de l'Espaceaeroelasticity; non-linear aerodynamics; flutterAEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies4
Gabriel Barreau; François Pechereau; Philippe Lalande; Frédéric Alauzet; Guillaume Puigt3D modeling of a continuous arc with anisotropic mesh adaptationONERAMHD; CFD; Mesh adaptation; electric arcCFDMPS - CFD & Multi-Physics Simulation in Aerospace5
François Pechereau; Fabien Tholin; Julien Vanharen; Guillaume Puigt; Frédéric Alauzet and Philippe Lalande3D Modeling of an arc in interaction with composite materialsONERACFD; LIGHTNING; PLASMA; CFRP; MESH ADAPTATIONCFDMPS - CFD & Multi-Physics Simulation in Aerospace6
Immo Huismann; Stefan FechterHyperCODA -- Stabilization methods for hypersonic flowsDeutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)CFD; hypersonic flow; finite volume method; numerical softwareCFDMPS - CFD & Multi-Physics Simulation in Aerospace7
Kevin Marangi; Flavio NocaComputational Fluid Dynamics of a Supersonic Rocket's AscentEPFL Rocket TeamSupersonic; CFD; drag minimization; rocket; compressible flowsCFDMPS - CFD & Multi-Physics Simulation in Aerospace8
Alessia Assonitis; Renato Paciorri; Enrico Cavallini; Simone Illiano; Simone Pizzurro; Simone Ciabuschi3D flow simulations of space launchers stage separations through overset approachUniversity of Rome La Sapienzaspace launchers; overset method; stage separationCFDMPS - CFD & Multi-Physics Simulation in Aerospace9
Yeontaek Jung; Hanna Lee; Youngjun Lee; Youdan KimExplicit Midcourse Guidance Law of Multi-stage Anti-ballistic Missile with Solid PropellantSeoul National UniversityAnti-ballistic missile; Midcourse guidance; Solid propellant; Explicit guidanceFDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications10
Can Öznurlu; Berke Bayr?; Farhat AsimLateral-Directional Control Law Design, Handling Qualities and Uncertainty Analysis for a Re-entry Vehicle HL-20 Flight Control SystemTurkish AerospaceControl; Handling Quality; Flying Quality; Re-entry; UncertaintyFDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications11
Qiao Li; Xingchen Li; Wen YaoField reconstruction of the spacecraft from limited sensors based on graph neural networks.National University of Defense TechnologyField reconstruction; graph neural networksFDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications12
Xuxing Huang; Bin Yang; Shuang LiIntelligent guidance method for Galilean moon cycling with online error fitting via reinforcement learningNanjing University of Aeronautics and AstronauticsGalilean moon cycling; intelliigent guidance; error fitting; reinforcement learningFDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications13
Xin Zhang; Jiyuan Sun; Shushi WangRobust Adaptive Switching Control of Hypersonic Reentry Vehicle based on Q-learningAcademy of Astronautics. Nanjing University of Aeronautcs & AstronauticsFDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications14
Carlo E.D. Riboldi; Marco TomasoniDynamic Simulation, Flight Control and Guidance Synthesis for Fixed-Wing UAV SwarmsDAER - Politecnico di Milanoswarm; uav; formation flight; coordination; leader-follower; nonlinear simulation; stability augmentation; guidance; beam tracking; altitude tracking; fixed-wing uav; droneFDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications15
Sevket Utku AYDINLI; Yagiz KURT; Halil Ersin SOKEN; Ali Turker KUTAYApplication of Vision Based Target Tracking and Motion Planning Algorithms in Dynamic EnvironmentMiddle East Technical UniversityMotion Planning; Target Tracking; Mobile Robots; Multi-Robot Systems; Deep Reinforcement LearningFDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications16
Sevket Utku AYDINLI; Ali Turker KUTAYSimultaneous Arrival Strategy by Using Learning-Based ApproachMiddle East Technical UniversitySimultaneous Arrival; Cooperative Guidance; Control Guidance; Deep Reinforcement Learning; Missile Guidance FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications17
Hongyu Qiao; Shuanghou Deng; Fan Qing; Tianhang XiaoA Numerical Virtual Flight Platform Development and its Application on High Maneuverability Flight VehiclesNanjing University of Aeronautics and AstronauticsNumerical Virtual Flight; High ManeuverabilityFDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications18
Huimin Xiang;Qingzhen Yang;Xufei Wang;Jiazheng FanStudy on the Influence of Vortex Generator on Aerodynamic and Stealth Characteristics of Serpentine InletNorthwestern Polytechnical University Serpentine inlet; Vortex Generator; aerodynamic performance;electromagnetic scattering characteristicsFLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies19
Elias; Khiar; Severac; Morilhat; Luyssen; Tobeli; Bur; Doudet; Wattellier; Bizet; André; Mahieu; Mysyrowicz; HouardRepetitive Femtosecond Laser Energy deposition for Supersonic Flow ControlONERALaser; Supersonic; energy deposition; femtosecondFLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies20
Roberto Andriani; Antonella IngenitoPerformance Analysis of a Hybrid Thermal-Electric Turboprop EnginePolitecnico di MilanoHybrid; Thermal; Electric; TurbopropHEPAEM - Hybrid Electric Propulsion21
Raphaël Chirac; Herimanana Zafiharimalala; Arturo Martinez-Gracida; Franck Cazaurang; Jean-Marc Andre Validation of a hazard taxonomy with aviation maintenance expertsHuman design GroupAircraft maintenance; hazards taxonomy; safetyHUMANF - Human factors in Aviation and Space23
Ye Xiao; Xingchen Li; Wen Yao; Yi XiaoFRA-GRU: A Deep Learning model for vessel trajectory prediction based on satellite AIS dataHunan UniversityAutomatic Identification System (AIS); maritime transport; gated recurrent unit (GRU); vessel trajectory predictionNEWSPA - New systems for future space operations24
Alexander Koehler; Marcus T. KnoppFirst operational tests with the optical ground station at TrauenGerman Aerospace CenterFree-space optical communications; optical ground station; laser-communication; direct-to-Earth laser link; optical LEO downlinksNEWSPA - New systems for future space operations25
Louis-Ashley CAMUS From Visual Inspections to AI-Driven Checks: Automating Quadrant Star Sensor Calibration Space OperationsOneWebArtificial Intelligence; Space operations; Quadrant Star Sensor; AutomationNEWSPA - New systems for future space operations26
Manami FUJII; Tetsuya SATO; Atsushi HASHIMOTO; Hideyuki TAGUCHIPressure Model of Buzz Oscillation in a Ramjet IntakeWaseda UniversityRamjet Intake; Buzz; CFD; supersonicPROPHY - Propulsion Physics for Aeronautic and Space Applications27
Oh-Sung Kwon; Joong-Youp LeeLOX recirculation characteristics of propellant feeding system with a filter installed at tank outletKARILOX Recirculation; Propellant Feeding System; Cryogenic PropellantPROPHY - Propulsion Physics for Aeronautic and Space Applications28
John Cater; Max Goddard-Winchester; Xiyong Huang; Nick Long; Ben Mallett; Jamal Olatunji; Betina Pavri; Randy POLLOCK; Avinash Rao; Nick Rattenbury; Cameron Shellard; Nick Strickland; David WrightThe Hēki Mission: Testing Superconducting Magnet Technology for Space Propulsion on the International Space StationRobinson Research InstituteElectric Propulsion; High Temperature Superconductors; AF-MPDPROPHY - Propulsion Physics for Aeronautic and Space Applications29
Ibraheem Nasser; Chiara Manfletti; Tiziano Santese ; Oskar HaidnNumerical investigation on heat transfer of Rocket Engine Cooling Channel for different LNG Under Trans and Super-Critical ConditionsTUMCooling Channel; LNG; Supercritical Pressure; Liquid Rocket EnginePROPHY - Propulsion Physics for Aeronautic and Space Applications30
Ruyao Wang; Junwei Li; Deyou Wang; Jiajin Zeng; Ningfei WangExperimental study of pulsed triggering oscillation in T-burnerBeijing Institute of Technologypulse triggering; T-burner; pressure oscillation; solid rocket motorPROPHY - Propulsion Physics for Aeronautic and Space Applications31
Eliot SIDOMMO; Washington GEORGESInnovative propulsion technologies for increased CubeSat efficiencyIPSA ONEionic propulsion; plasma; grid thruster; rail launcherPROPHY - Propulsion Physics for Aeronautic and Space Applications32
Seongmin Joo; Dokeun Hwang; Donghyuk Kang; Seongchan Heo; Sanghoon Han; Byeongyoung Lee; Wonju Je; Jonggyu KimCold flow test of pintle injector for variable thrust combustion chamber with servo-valve methodKorea Aerospace Research InstituteCold flow test; Pintle injector; Servo-valve; Variable thrustPROPHY - Propulsion Physics for Aeronautic and Space Applications33
Musa Onur ÖZTÜRKMEN; Yusuf ÖZYÖRÜKStability Characteristics of a Single Injector Combustor through Acoustic Solutions with Large Eddy Simulated Heat SourcesMiddle East Technical UniversityHelmholtz solver; thermo-acoustic instabilities; flame transfer functionPROPHY - Propulsion Physics for Aeronautic and Space Applications34
Prasanth P Nair; Vinod NarayananNumerical simulation of the effect of different divergent angle of pylonIIT Gandhinagarscramjet; cavity-based; pylon; DMD; IDDESPROPHY - Propulsion Physics for Aeronautic and Space Applications35
Kakeru Mizukoshi; Noritaka Sako; Jun Hayashi; Yu Daimon; Hiroshi KawanabeEffect of surface roughness on jet impingement cooling of a superheated wallKyoto UniversityJet impingement cooling; Liquid film; Surface roughness; Heat transferPROPHY - Propulsion Physics for Aeronautic and Space Applications36
Etienne Gourcerol; Victor Désangles; Denis Packan; Freddy GaboriauDesign of a 2-axis thrust stand for thrust vectoring diagnostics of an ECR thrusterONERAElectric propulsion; ECR thruster; thrust vectoring; 2-axis thrust standPROPHY - Propulsion Physics for Aeronautic and Space Applications37
Seungho Lee; Sunho Lee; Jaehyuk Huh; Sejin KwonProposal of Aerospace-informatics by Design of Ramjet Inlet Using Machine LearningKorea Advanced Institute of Science and Technology (KAIST)Aerospace-informatics; Ramjet; Inlet; Machine LearningPROPHY - Propulsion Physics for Aeronautic and Space Applications38
Jian Cheng; Jinle Cao; Yinghua Ye; Ruiqi ShenMicrowave controlled ignition, combustion and extinguishment characteristics of ADN-based ionic liquid propellant in single mode resonatorNanjing University of Science and TechnologyADN; ionic liquid propellant; microwave controlled propulsion; microwave ignitionPROPHY - Propulsion Physics for Aeronautic and Space Applications39
Konstantinos KATSONIS; Chloe BERENGUERISRU electric propulsion in the Neptune vicinityDEDALOS LtdISRU; Solar System; H2/He propellantPROPHY - Propulsion Physics for Aeronautic and Space Applications40
Abhijit Pamarty; Craig Mascarenhas; James AndersonMulti-objective optimization as a preliminary analysis tool for the design of airborne scientific instrumentsHarvard Universitymultiobjective optimization; genetic algorithm; solar-powered aircraft; atmospheric instrumentationPROPHY - Propulsion Physics for Aeronautic and Space Applications41
Ivens Daniel Hoffmann; Dmitry Suslov; Jan Deeken; Justin HardiInvestigation on Pressure Loss and Spray Angle on Different 3D-Printed Helical Swirl InjectorsGerman Aerospace Center (DLR)Helical Swirler; Pressure Loss; Spray AnglePROPHY - Propulsion Physics for Aeronautic and Space Applications42
Hongsheng Yu; Xiaodong Yu; Hongwei Gao; Wei Zhang; Luigi T. DeLuca; Ruiqi ShenUsing metal oxides to reduce pyrolysis difficulty for getting weaken-bond HTPB-based hybrid rocket fuelsNanjing University of Science and Technologyhybrid rocket propulsion; fuel; weaken-bond HTPB; catalysts; combustion PROPHY - Propulsion Physics for Aeronautic and Space Applications43
Davide Cavalieri; Jacopo Liberatori; Pasquale Eduardo Lapenna; Pietro Paolo CiottoliA multi-component droplet vaporization model for non-ideal fluidsSapienza Università di RomaDroplet vaporization; multi-component; non-ideal fluidsPROPHY - Propulsion Physics for Aeronautic and Space Applications44
Craig Anderson; Christopher NelsonChallenges of developing commercial activity on the moonN/Amoon colonization; lunar challengesSPEXPLO - Space Exploration - In Situ Resource Utilization45
Yeonhi Kim; Jungsun ParkOptimal design of three-dimensional woven composite aircraft wing with genetic algorithmthree-dimensional woven composite; aircraft wing; optimal design; genetic algorithmSTRMAT - Structures & Materials for Aeronautic and Space Systems46
Urara Kamon; Shugo Date; Keiichi Shirasu; Yoshiaki Kawagoe; Kazuki Ryuzono; Tomonaga OkabeThe effect of hot/wet environment on the structural weight of aircraft wing using thermoplastic CFRPTohoku UniversityCarbon fiber reinforced plastic; Aircraft wing; Static aeroelasticitySTRMAT - Structures & Materials for Aeronautic and Space Systems47
Charalampos KosmasLunar cargo (Oversized or Parcels) LUNAR CARGO P.C.Lunar Cargo; Oversized Cargo; ParcelsSTRMAT - Structures & Materials for Aeronautic and Space Systems48
Vint Lee; Sohom RoyLow-cost, Lightweight Electronic Flow Regulators for Throttling Liquid Rocket EnginesUC Berkeleyliquid rocket engine; reusable rocket; pressure regulator; flow regulator; thrust control; variable-thrust rocket; closed-loop controlSTUDENT - Space Student Projects50
Ayushi Pandya Benefits of Boundary Layer Ingestion with Froude's Propeller TheoryENSMABoundary Layer Ingestion SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations51
Ryohei CHINO; Yoshiaki KAWAGOE; Shugo DATE; Kazuki RYUZONO; Tomonaga OKABEInvestigation of weight estimation in conceptual design for composite aircraft developmentTohoku UniversityConceptual Design of Aircraft; FSI; Composite Materials; SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations52
Sultan Alyammahi; Hamad Albalooshi; Talal Alyaqubi; Mohammed Alhammadi ; Mohammed Alhammadi; Sheharyar MalikMoveable winglets on the wing of the aircraftAdpolyWinglets; induced drag; moveable wing tip; drag reduction; novel wing tip Winglets; induced drag; moveable wing tip; drag reduction; novel wing tip SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations53
Valery Frolov; Mikhail Medvedsky; Vadym Naumov; Petro Smertenko; Arnolds Ubelis; Vidvuds BeldavsCurrent problems of modeling and monitoring of near-earth orbital debris population for the safety of the future space missionsNational Academy of Sciences of Ukraineaerospace technology; space debris; remote sensing; environmental monitoring; mathematical modelingSUSTSP - Sustainable Space: Logistics and Space Debris54
Brandon Israel Escamilla Estrada;Giuseppe Di Pasquale;Daniel Gonzalez Arribas;Daniel Pérez Grande;Manuel Sanjurjo-RivoA Concurrent Methodology for Optimizing Constellation Deployment and Launcher SelectionUniversidad Carlos III de MadridSUSTSP - Sustainable Space: Logistics and Space Debris55
Masashi Miura ; Yuki SakamotoInteractive System Modeling for Designing a New Concept Launch VehicleJAXA/ISASSystem Model; System Design; ModelingSYSINT - System-Integration on Aircraft and Space Systems56
Mitchell Galletly; Allen Chan; Dries VerstraeteDesign Optimisation and Comparison of Propulsion Systems for Sounding Rockets University of SydneySYSINT - System-Integration on Aircraft and Space Systems57
Jiri CecrdleAeroelastic Demonstrator and Methodology for Experimental Investigation of Propeller Aerodynamic DerivativesCzech Aerospace Research Centre (VZLU)whirl flutter; aerodynamic derivative; W-STING demonstratorTESTING - Testing in Aerospace58
JONGMIN KIMWeight reduction of TPS and insulation material by using thermal conductivity in vacuum conditionKorea Aerospace Research Institutevacuum; insulation; thermal conductivity; TPSTESTING - Testing in Aerospace59
Granger Florian; Airiau Magdeleine; Devillers Robin; Dorey Luc-Henry; Zuzio Davide; Estivalezes Jean-LucVolume estimation on ombroscopy images using deep learning and high fidelity simulationsCNES/ONERADeep learning; high fidelity simulations; volume estimation; two-phase flows; assisted atomizationTESTING - Testing in Aerospace60
Angelo Pasini; Stefano Calatafimi; Elia Puccinelli; Tommaso GerbiAtmospheric Test Campaign of a Hydrogen Peroxide Propulsion System for CubeSatsUniversity of PisaGreen propellants; chemical propulsion system; hydrogen peroxide; test campaign; CubeSats; monopropellantTESTING - Testing in Aerospace61
Seong Min JeonInvestigation on Active Axial Thrust Balancing for a TurbopumpKorea Aerospace Research InstituteRocket engine; Turbopump; Axial thrust; Active balancingTURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO)62
Karol B?ben; Robert G??bockiComparison of evolutionary algorithms for optimizing the flight path of a Unmanned Aerial Vehicles swarm?ukasiewicz - Institute of AviationUAV Swarm; Evolutionary algorithms; Path planningUAVFUT - UAVs: Future Applications/Services and Specific Technologies63
Longobardi Pasquale; Skaloud JanWind Tunnel Characterization of a Delta-Wing UAV for Model-Based NavigationEPFLUAV; Wind Tunnel; Aerodynamics; Autonomous; Model-based navigation NavigationUAVFUT - UAVs: Future Applications/Services and Specific Technologies64
Arrigo AVI; Giuseppe QUARANTA; Riccardo PARINUAV icing testing facility for H24 servicesEuracUAV; Ice tunnel; Ice accretion; system characterizationUAVFUT - UAVs: Future Applications/Services and Specific Technologies65
R?zvan-Ionu? B?LA?A; Marian-Ciprian BÎLU; C?t?lin IORDACHE A Reinforcement Learning approach to UAV trajectory configuration National Institute for Aerospace Research "Elie Carafoli" - INCASUAV; Reinforcement Learning; Proximal Policy Optimization; Trajectory OptimizationUAVFUT - UAVs: Future Applications/Services and Specific Technologies67
Dominik Reinhardt; Dr. Abdessalem BouferroukA Simplified Digital Twin Framework of a Trainer Aircraft to Enhance Flight TestingUWE BristolFDGNCAV; SUSTAV; UAVFUTUAVFUT - UAVs: Future Applications/Services and Specific Technologies68
Boubakr ZEBIRI *; Nassim BRAHMI; Abdellah HADJADJ Effects of wall temperature on turbulent boundary layer separation in supersonic planar nozzlesINSA RouenNozzle Flow Separation; Heat transfer; Shock-Boundary Supersonic Layer Interaction; Low-frequency shock Oscillations; Large-Eddy Simulation)PROPHY - Propulsion Physics for Aeronautic and Space Applications69
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