| Aircraft design and testing of FLEXOP unmanned flying demonstrator to test load alleviation and flutter suppression of high aspect ratio flexible wings C Roessler, P Stahl, F Sendner, A Hermanutz, S Koeberle, ... AIAA scitech 2019 forum, 1813, 2019 | 34 | 2019 |
| Active flutter mitigation testing on the FLEXOP demonstrator aircraft B Takarics, B Patartics, T Luspay, B Vanek, C Roessler, J Bartasevicius, ... AIAA Scitech 2020 Forum, 1970, 2020 | 25 | 2020 |
| Experimental investigation of high-incidence delta-wing flow control A Buzica, J Bartasevicius, C Breitsamter Experiments in Fluids 58 (9), 131, 2017 | 14 | 2017 |
| Results of an Aeroelastically Tailored Wing on the FLEXOP Demonstrator Aircraft C Roessler, J Bartasevicius, SJ Koeberle, D Teubl, M Hornung, ... AIAA Scitech 2020 Forum, 1969, 2020 | 11 | 2020 |
| Ground testing of the flexop demonstrator aircraft J Sodja, R De Breuker, YM Meddaikar, JK Dillinger, K Soal, Y Govers, ... AIAA Scitech 2020 Forum, 1968, 2020 | 11 | 2020 |
| Flight testing of 65kg t-flex subscale demonstrator J Bartasevicius, SJ Koeberle, D Teubl, C Roessler, M Hornung 32nd Congress of the International Council of the Aeronautical Sciences, 2021 | 9 | 2021 |
| Comparing potential flow solvers for aerodynamic characteristics estimation of the T-Flex UAV F Yu, J Bartasevicius, M Hornung ICAS, 2022 | 7 | 2022 |
| Flight vibration testing of the t-flex uav using online modal analysis K Soal, R Volkmar, C Thiem, J Sinske, YM Meddaikar, Y Govers, ... AIAA Scitech 2023 Forum, 0373, 2023 | 6 | 2023 |
| Discrete vortices on delta wings with unsteady leading-edge blowing J Bartasevicius, A Buzica, C Breitsamter 8th AIAA Flow Control Conference, 3170, 2016 | 6 | 2016 |
| Aeroservoelastic induced drag modelling and minimization for the T-FLEX demonstrator YM Meddaikar, TM Kier, J Bartasevicius, F Yu, B Vanek, A Olgyay, ... AIAA Scitech 2023 Forum, 0176, 2023 | 4 | 2023 |
| Active vortex flow control on a generic delta wing A Buzica, J Bartasevicius, C Breitsamter Proceedings of the 30th Congress of ICAS, Daejon, South Korea, 2016 | 3 | 2016 |
| Design and testing of an in-flight thrust measurement system for a pylon-mounted miniature jet engine J Bartasevicius, PA Fleig, A Metzner, M Hornung AIAA SCITECH 2022 Forum, 1827, 2022 | 2 | 2022 |
| In-flight drag measurement and validation for a medium-sized UAV J Bartasevicius, M Hornung AIAA SCITECH 2023 Forum, 0372, 2023 | 1 | 2023 |
| Contribution of the ground vibration tests for the preparation of flutter suppression flight test campaigns: case of the FliPASED P-FLEX UAV N Guérin, C Stephan, P Lubrina, K Soal, M Tang, R Volkmar, Y Govers, ... IFASD 2024, 2024 | | 2024 |
| LESSONS LEARNED FROM FLIGHT TESTING ACTIVE FLUTTER SUPPRESSION TECHNOLOGIES J Bartasevicius, D Teubl, T Seren, F Yu, M Hornung, B Vanek, D Balogh, ... | | |
| D3. 2 Flight Test Report Phase J Bartasevicius | | |
Mirko HornungProfessor for Aircraft Design, Technische Universität MünchenBestätigte E-Mail-Adresse bei tum.de
