Poster Presentations

  • Numerical Investigation of Flexible Flapping Wing Propulsion at Low-Reynolds Numbers
    Shuanghou Deng, Wee-Beng Tay, B.W.Oudeheusden, Hester Bijl, Technology University of Delft, the Netherlands, Tianhang Xiao, Nanjing University of Aeronautics and Astronautics, PR China

  • Flight Simulation and Control of a Tailless Flapping Wing MAV near Hover
    Matěj Karásek, André Preumont, Université Libre de Bruxelles, Belgium

  • Validation and numerical simulation using the immersed boundary method solvers for flapping wing flight
    Wee-Beng Tay, Delft University of Technology, The Netherlands

  • Vortex Structure around Moving Elastic Bodies by Fluid Structure Interaction Simulation
    Tetsushi Nagata, Kyushu Institute of Technology, Japan

  • Towards an Open-Source ROS-Compliant AVR Software Autopilot Platform
    Marcin Kmiecik, Krzysztof Sibilski, Wroclaw University of Technology, Poland

  • Neural Model of Unsteady Aerodynamic Coefficients of MAV from Water Tunnel Test Data
    Michal Garbowski, Krzysztof Sibilski,     Wroclaw University of Technology, Poland

  • FSR UAV Robotics Team
    Mohammad Nikkhah, Iman Shirdareh, Ramin Marhamati, Mohsen Afshari, Alireza Riyazi, Islamic Azad University, Fars, Iran

  • Design and Wind Tunnel Testing of an Active Morphing Wing Ornithopter
    Wenbo Duan, Haisong Ang, Nanjing University of Aeronautics and Astronautics, P.R. China

  • Numerical Investigation of Azarakhsh MAV
    Mohammadreza Radmanesh, Sayed Amin Feghhi,     Isfahan University of Technology, IRAN

  • A new method for design of Fixed Wing Micro Air Vehicle
    Mostafa Hassanalian, Mahmud Ashrafizaadeh, Saeed Ziaei-Rad, Isfahan University of Technology, Iran

  • Sending instructions and receiving the data from MAVs using telecommunication networks
    Mostafa Hassanalian,     Isfahan University of Technology, Iran

  • A New Quad-rotor Configuration for Improving Static Stability near Hovering
    Feng Ni, Hong Kong University of Science and Technology

  • Experimental Investigation on Aerodynamics Loads of an Entomopter in Forward Flight – Water Tunnel Tests
    Pawel Czekalowski, Krzysztof Sibilski, Wroclaw University of Technology, Poland

  • The Influence of Wing Design and Flapping Frequency on the four-dimensional Flow Pattern of a Model Wing at Bird Scale
    William Thielicke, Eize J. Stammhuis, University of Groningen, The Netherlands, Antonia B. Kesel, University of Applied Sciences Bremen, Germany

  • Onboard flight parameters registration system
    Vitaly Kobtsev, Sergey Levin, Sergey Serokhvostov, Nikita Ageev, Moscow Institute of Physics and Technology, DAFE, Russia


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