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.
| AUTHORS | TITLE | ORGANIZATION | KEYWORDS | TOPIC | SESSION |
|---|---|---|---|---|---|
| Deyou Wang; Ge Jin; Ruyao Wang; Shipeng Li | Flow separation characteristics of supersonic nozzles in water environment | Beijing Institute of Technology | Underwater jet propulsion; Supersonic nozzles; Flow separation; Water environment; Unsteady characteristics | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | 1 |
| Stoliaroff | Ariane 6 IMA Separation Test | Arianegroup | Separation; test; Ariane 6 | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | 2 |
| Benjamin Khiar; Fabien Tholin; François Pechereau; Denis Packan | Modelling of MHD flow control for atmospheric re-entry | ONERA | MHD; re-entry; flow control; hypersonic; magnetic field | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | 3 |
| Yann BLAIRON; Olivier MONTAGNIER; Annie LEROY | Dynamic stall models for post flutter analysis of an aeroelastic wing section | École de l'Air et de l'Espace | aeroelasticity; non-linear aerodynamics; flutter | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | 4 |
| Gabriel Barreau; François Pechereau; Philippe Lalande; Frédéric Alauzet; Guillaume Puigt | 3D modeling of a continuous arc with anisotropic mesh adaptation | ONERA | MHD; CFD; Mesh adaptation; electric arc | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | 5 |
| François Pechereau; Fabien Tholin; Julien Vanharen; Guillaume Puigt; Frédéric Alauzet and Philippe Lalande | 3D Modeling of an arc in interaction with composite materials | ONERA | CFD; LIGHTNING; PLASMA; CFRP; MESH ADAPTATION | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | 6 |
| Immo Huismann; Stefan Fechter | HyperCODA -- Stabilization methods for hypersonic flows | Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR) | CFD; hypersonic flow; finite volume method; numerical software | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | 7 |
| Kevin Marangi; Flavio Noca | Computational Fluid Dynamics of a Supersonic Rocket's Ascent | EPFL Rocket Team | Supersonic; CFD; drag minimization; rocket; compressible flows | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | 8 |
| Alessia Assonitis; Renato Paciorri; Enrico Cavallini; Simone Illiano; Simone Pizzurro; Simone Ciabuschi | 3D flow simulations of space launchers stage separations through overset approach | University of Rome La Sapienza | space launchers; overset method; stage separation | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | 9 |
| Yeontaek Jung; Hanna Lee; Youngjun Lee; Youdan Kim | Explicit Midcourse Guidance Law of Multi-stage Anti-ballistic Missile with Solid Propellant | Seoul National University | Anti-ballistic missile; Midcourse guidance; Solid propellant; Explicit guidance | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | 10 |
| Can Öznurlu; Berke Bayr?; Farhat Asim | Lateral-Directional Control Law Design, Handling Qualities and Uncertainty Analysis for a Re-entry Vehicle HL-20 Flight Control System | Turkish Aerospace | Control; Handling Quality; Flying Quality; Re-entry; Uncertainty | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | 11 |
| Qiao Li; Xingchen Li; Wen Yao | Field reconstruction of the spacecraft from limited sensors based on graph neural networks. | National University of Defense Technology | Field reconstruction; graph neural networks | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | 12 |
| Xuxing Huang; Bin Yang; Shuang Li | Intelligent guidance method for Galilean moon cycling with online error fitting via reinforcement learning | Nanjing University of Aeronautics and Astronautics | Galilean moon cycling; intelliigent guidance; error fitting; reinforcement learning | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | 13 |
| Xin Zhang; Jiyuan Sun; Shushi Wang | Robust Adaptive Switching Control of Hypersonic Reentry Vehicle based on Q-learning | Academy of Astronautics. Nanjing University of Aeronautcs & Astronautics | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | 14 | |
| Carlo E.D. Riboldi; Marco Tomasoni | Dynamic Simulation, Flight Control and Guidance Synthesis for Fixed-Wing UAV Swarms | DAER - Politecnico di Milano | swarm; uav; formation flight; coordination; leader-follower; nonlinear simulation; stability augmentation; guidance; beam tracking; altitude tracking; fixed-wing uav; drone | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | 15 |
| Sevket Utku AYDINLI; Yagiz KURT; Halil Ersin SOKEN; Ali Turker KUTAY | Application of Vision Based Target Tracking and Motion Planning Algorithms in Dynamic Environment | Middle East Technical University | Motion Planning; Target Tracking; Mobile Robots; Multi-Robot Systems; Deep Reinforcement Learning | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | 16 |
| Sevket Utku AYDINLI; Ali Turker KUTAY | Simultaneous Arrival Strategy by Using Learning-Based Approach | Middle East Technical University | Simultaneous Arrival; Cooperative Guidance; Control Guidance; Deep Reinforcement Learning; Missile Guidance | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | 17 |
| Hongyu Qiao; Shuanghou Deng; Fan Qing; Tianhang Xiao | A Numerical Virtual Flight Platform Development and its Application on High Maneuverability Flight Vehicles | Nanjing University of Aeronautics and Astronautics | Numerical Virtual Flight; High Maneuverability | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | 18 |
| Huimin Xiang;Qingzhen Yang;Xufei Wang;Jiazheng Fan | Study on the Influence of Vortex Generator on Aerodynamic and Stealth Characteristics of Serpentine Inlet | Northwestern Polytechnical University | Serpentine inlet; Vortex Generator; aerodynamic performance;electromagnetic scattering characteristics | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | 19 |
| Elias; Khiar; Severac; Morilhat; Luyssen; Tobeli; Bur; Doudet; Wattellier; Bizet; André; Mahieu; Mysyrowicz; Houard | Repetitive Femtosecond Laser Energy deposition for Supersonic Flow Control | ONERA | Laser; Supersonic; energy deposition; femtosecond | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | 20 |
| Roberto Andriani; Antonella Ingenito | Performance Analysis of a Hybrid Thermal-Electric Turboprop Engine | Politecnico di Milano | Hybrid; Thermal; Electric; Turboprop | HEPAEM - Hybrid Electric Propulsion | 21 |
| Raphaël Chirac; Herimanana Zafiharimalala; Arturo Martinez-Gracida; Franck Cazaurang; Jean-Marc Andre | Validation of a hazard taxonomy with aviation maintenance experts | Human design Group | Aircraft maintenance; hazards taxonomy; safety | HUMANF - Human factors in Aviation and Space | 23 |
| Ye Xiao; Xingchen Li; Wen Yao; Yi Xiao | FRA-GRU: A Deep Learning model for vessel trajectory prediction based on satellite AIS data | Hunan University | Automatic Identification System (AIS); maritime transport; gated recurrent unit (GRU); vessel trajectory prediction | NEWSPA - New systems for future space operations | 24 |
| Alexander Koehler; Marcus T. Knopp | First operational tests with the optical ground station at Trauen | German Aerospace Center | Free-space optical communications; optical ground station; laser-communication; direct-to-Earth laser link; optical LEO downlinks | NEWSPA - New systems for future space operations | 25 |
| Louis-Ashley CAMUS | From Visual Inspections to AI-Driven Checks: Automating Quadrant Star Sensor Calibration Space Operations | OneWeb | Artificial Intelligence; Space operations; Quadrant Star Sensor; Automation | NEWSPA - New systems for future space operations | 26 |
| Manami FUJII; Tetsuya SATO; Atsushi HASHIMOTO; Hideyuki TAGUCHI | Pressure Model of Buzz Oscillation in a Ramjet Intake | Waseda University | Ramjet Intake; Buzz; CFD; supersonic | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 27 |
| Oh-Sung Kwon; Joong-Youp Lee | LOX recirculation characteristics of propellant feeding system with a filter installed at tank outlet | KARI | LOX Recirculation; Propellant Feeding System; Cryogenic Propellant | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 28 |
| 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 Wright | The Hēki Mission: Testing Superconducting Magnet Technology for Space Propulsion on the International Space Station | Robinson Research Institute | Electric Propulsion; High Temperature Superconductors; AF-MPD | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 29 |
| Ibraheem Nasser; Chiara Manfletti; Tiziano Santese ; Oskar Haidn | Numerical investigation on heat transfer of Rocket Engine Cooling Channel for different LNG Under Trans and Super-Critical Conditions | TUM | Cooling Channel; LNG; Supercritical Pressure; Liquid Rocket Engine | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 30 |
| Ruyao Wang; Junwei Li; Deyou Wang; Jiajin Zeng; Ningfei Wang | Experimental study of pulsed triggering oscillation in T-burner | Beijing Institute of Technology | pulse triggering; T-burner; pressure oscillation; solid rocket motor | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 31 |
| Eliot SIDOMMO; Washington GEORGES | Innovative propulsion technologies for increased CubeSat efficiency | IPSA ONE | ionic propulsion; plasma; grid thruster; rail launcher | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 32 |
| Seongmin Joo; Dokeun Hwang; Donghyuk Kang; Seongchan Heo; Sanghoon Han; Byeongyoung Lee; Wonju Je; Jonggyu Kim | Cold flow test of pintle injector for variable thrust combustion chamber with servo-valve method | Korea Aerospace Research Institute | Cold flow test; Pintle injector; Servo-valve; Variable thrust | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 33 |
| Musa Onur ÖZTÜRKMEN; Yusuf ÖZYÖRÜK | Stability Characteristics of a Single Injector Combustor through Acoustic Solutions with Large Eddy Simulated Heat Sources | Middle East Technical University | Helmholtz solver; thermo-acoustic instabilities; flame transfer function | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 34 |
| Prasanth P Nair; Vinod Narayanan | Numerical simulation of the effect of different divergent angle of pylon | IIT Gandhinagar | scramjet; cavity-based; pylon; DMD; IDDES | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 35 |
| Kakeru Mizukoshi; Noritaka Sako; Jun Hayashi; Yu Daimon; Hiroshi Kawanabe | Effect of surface roughness on jet impingement cooling of a superheated wall | Kyoto University | Jet impingement cooling; Liquid film; Surface roughness; Heat transfer | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 36 |
| Etienne Gourcerol; Victor Désangles; Denis Packan; Freddy Gaboriau | Design of a 2-axis thrust stand for thrust vectoring diagnostics of an ECR thruster | ONERA | Electric propulsion; ECR thruster; thrust vectoring; 2-axis thrust stand | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 37 |
| Seungho Lee; Sunho Lee; Jaehyuk Huh; Sejin Kwon | Proposal of Aerospace-informatics by Design of Ramjet Inlet Using Machine Learning | Korea Advanced Institute of Science and Technology (KAIST) | Aerospace-informatics; Ramjet; Inlet; Machine Learning | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 38 |
| Jian Cheng; Jinle Cao; Yinghua Ye; Ruiqi Shen | Microwave controlled ignition, combustion and extinguishment characteristics of ADN-based ionic liquid propellant in single mode resonator | Nanjing University of Science and Technology | ADN; ionic liquid propellant; microwave controlled propulsion; microwave ignition | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 39 |
| Konstantinos KATSONIS; Chloe BERENGUER | ISRU electric propulsion in the Neptune vicinity | DEDALOS Ltd | ISRU; Solar System; H2/He propellant | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 40 |
| Abhijit Pamarty; Craig Mascarenhas; James Anderson | Multi-objective optimization as a preliminary analysis tool for the design of airborne scientific instruments | Harvard University | multiobjective optimization; genetic algorithm; solar-powered aircraft; atmospheric instrumentation | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 41 |
| Ivens Daniel Hoffmann; Dmitry Suslov; Jan Deeken; Justin Hardi | Investigation on Pressure Loss and Spray Angle on Different 3D-Printed Helical Swirl Injectors | German Aerospace Center (DLR) | Helical Swirler; Pressure Loss; Spray Angle | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 42 |
| Hongsheng Yu; Xiaodong Yu; Hongwei Gao; Wei Zhang; Luigi T. DeLuca; Ruiqi Shen | Using metal oxides to reduce pyrolysis difficulty for getting weaken-bond HTPB-based hybrid rocket fuels | Nanjing University of Science and Technology | hybrid rocket propulsion; fuel; weaken-bond HTPB; catalysts; combustion | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 43 |
| Davide Cavalieri; Jacopo Liberatori; Pasquale Eduardo Lapenna; Pietro Paolo Ciottoli | A multi-component droplet vaporization model for non-ideal fluids | Sapienza Università di Roma | Droplet vaporization; multi-component; non-ideal fluids | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 44 |
| Craig Anderson; Christopher Nelson | Challenges of developing commercial activity on the moon | N/A | moon colonization; lunar challenges | SPEXPLO - Space Exploration - In Situ Resource Utilization | 45 |
| Yeonhi Kim; Jungsun Park | Optimal design of three-dimensional woven composite aircraft wing with genetic algorithm | three-dimensional woven composite; aircraft wing; optimal design; genetic algorithm | STRMAT - Structures & Materials for Aeronautic and Space Systems | 46 | |
| Urara Kamon; Shugo Date; Keiichi Shirasu; Yoshiaki Kawagoe; Kazuki Ryuzono; Tomonaga Okabe | The effect of hot/wet environment on the structural weight of aircraft wing using thermoplastic CFRP | Tohoku University | Carbon fiber reinforced plastic; Aircraft wing; Static aeroelasticity | STRMAT - Structures & Materials for Aeronautic and Space Systems | 47 |
| Charalampos Kosmas | Lunar cargo (Oversized or Parcels) | LUNAR CARGO P.C. | Lunar Cargo; Oversized Cargo; Parcels | STRMAT - Structures & Materials for Aeronautic and Space Systems | 48 |
| Vint Lee; Sohom Roy | Low-cost, Lightweight Electronic Flow Regulators for Throttling Liquid Rocket Engines | UC Berkeley | liquid rocket engine; reusable rocket; pressure regulator; flow regulator; thrust control; variable-thrust rocket; closed-loop control | STUDENT - Space Student Projects | 50 |
| Ayushi Pandya | Benefits of Boundary Layer Ingestion with Froude's Propeller Theory | ENSMA | Boundary Layer Ingestion | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | 51 |
| Ryohei CHINO; Yoshiaki KAWAGOE; Shugo DATE; Kazuki RYUZONO; Tomonaga OKABE | Investigation of weight estimation in conceptual design for composite aircraft development | Tohoku University | Conceptual Design of Aircraft; FSI; Composite Materials; | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | 52 |
| Sultan Alyammahi; Hamad Albalooshi; Talal Alyaqubi; Mohammed Alhammadi ; Mohammed Alhammadi; Sheharyar Malik | Moveable winglets on the wing of the aircraft | Adpoly | Winglets; 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 Operations | 53 |
| Valery Frolov; Mikhail Medvedsky; Vadym Naumov; Petro Smertenko; Arnolds Ubelis; Vidvuds Beldavs | Current problems of modeling and monitoring of near-earth orbital debris population for the safety of the future space missions | National Academy of Sciences of Ukraine | aerospace technology; space debris; remote sensing; environmental monitoring; mathematical modeling | SUSTSP - Sustainable Space: Logistics and Space Debris | 54 |
| Brandon Israel Escamilla Estrada;Giuseppe Di Pasquale;Daniel Gonzalez Arribas;Daniel Pérez Grande;Manuel Sanjurjo-Rivo | A Concurrent Methodology for Optimizing Constellation Deployment and Launcher Selection | Universidad Carlos III de Madrid | SUSTSP - Sustainable Space: Logistics and Space Debris | 55 | |
| Masashi Miura ; Yuki Sakamoto | Interactive System Modeling for Designing a New Concept Launch Vehicle | JAXA/ISAS | System Model; System Design; Modeling | SYSINT - System-Integration on Aircraft and Space Systems | 56 |
| Mitchell Galletly; Allen Chan; Dries Verstraete | Design Optimisation and Comparison of Propulsion Systems for Sounding Rockets | University of Sydney | SYSINT - System-Integration on Aircraft and Space Systems | 57 | |
| Jiri Cecrdle | Aeroelastic Demonstrator and Methodology for Experimental Investigation of Propeller Aerodynamic Derivatives | Czech Aerospace Research Centre (VZLU) | whirl flutter; aerodynamic derivative; W-STING demonstrator | TESTING - Testing in Aerospace | 58 |
| JONGMIN KIM | Weight reduction of TPS and insulation material by using thermal conductivity in vacuum condition | Korea Aerospace Research Institute | vacuum; insulation; thermal conductivity; TPS | TESTING - Testing in Aerospace | 59 |
| Granger Florian; Airiau Magdeleine; Devillers Robin; Dorey Luc-Henry; Zuzio Davide; Estivalezes Jean-Luc | Volume estimation on ombroscopy images using deep learning and high fidelity simulations | CNES/ONERA | Deep learning; high fidelity simulations; volume estimation; two-phase flows; assisted atomization | TESTING - Testing in Aerospace | 60 |
| Angelo Pasini; Stefano Calatafimi; Elia Puccinelli; Tommaso Gerbi | Atmospheric Test Campaign of a Hydrogen Peroxide Propulsion System for CubeSats | University of Pisa | Green propellants; chemical propulsion system; hydrogen peroxide; test campaign; CubeSats; monopropellant | TESTING - Testing in Aerospace | 61 |
| Seong Min Jeon | Investigation on Active Axial Thrust Balancing for a Turbopump | Korea Aerospace Research Institute | Rocket engine; Turbopump; Axial thrust; Active balancing | TURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO) | 62 |
| Karol B?ben; Robert G??bocki | Comparison of evolutionary algorithms for optimizing the flight path of a Unmanned Aerial Vehicles swarm | ?ukasiewicz - Institute of Aviation | UAV Swarm; Evolutionary algorithms; Path planning | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | 63 |
| Longobardi Pasquale; Skaloud Jan | Wind Tunnel Characterization of a Delta-Wing UAV for Model-Based Navigation | EPFL | UAV; Wind Tunnel; Aerodynamics; Autonomous; Model-based navigation Navigation | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | 64 |
| Arrigo AVI; Giuseppe QUARANTA; Riccardo PARIN | UAV icing testing facility for H24 services | Eurac | UAV; Ice tunnel; Ice accretion; system characterization | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | 65 |
| 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" - INCAS | UAV; Reinforcement Learning; Proximal Policy Optimization; Trajectory Optimization | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | 67 |
| Dominik Reinhardt; Dr. Abdessalem Bouferrouk | A Simplified Digital Twin Framework of a Trainer Aircraft to Enhance Flight Testing | UWE Bristol | FDGNCAV; SUSTAV; UAVFUT | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | 68 |
| Boubakr ZEBIRI *; Nassim BRAHMI; Abdellah HADJADJ | Effects of wall temperature on turbulent boundary layer separation in supersonic planar nozzles | INSA Rouen | Nozzle Flow Separation; Heat transfer; Shock-Boundary Supersonic Layer Interaction; Low-frequency shock Oscillations; Large-Eddy Simulation) | PROPHY - Propulsion Physics for Aeronautic and Space Applications | 69 |