First author publications:
Bartasevicius, J., & Hornung, M. (2023). In-flight drag measurement and validation for a medium-sized UAV. AIAA SCITECH 2023 Forum, January. https://doi.org/10.2514/6.2023-0372
Bartasevicius, J., & Hornung, M. (2023). Flight testing for flutter - operational design and lessons learned. SFTE 2023 International Symposium. https://www.researchgate.net/publication/
Bartasevicius, J., Alexandre, P., Fleig, T., Metzner, A., & Hornung, M. (2022). Design and testing of an in-flight thrust measurement system for a pylon-mounted miniature jet engine. https://doi.org/10.2514/6.2022-1827
Bartasevicius, J., Koeberle, S. J., Teubl, D., Roessler, C., & Hornung, M. (2021). Flight Testing of 65Kg T-Flex Subscale Demonstrator. 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021. https://www.icas.org/
Bartasevicius, J., Buzica, A., & Breitsamter, C. (2016). Discrete vortices on delta wings with unsteady leading-edge blowing. 8th AIAA Flow Control Conference. https://doi.org/10.2514/6.2016-3170
Others:
Soal, K., Volkmar, R., Thiem, C., Sinske, J., Meddaikar, Y. M., Govers, Y., Böswald, M., Teubl, D., Bartasevicius, J., Nagy, M., & Vanek, B. (2023). Flight Vibration Testing of the T-FLEX UAV using Online Modal Analysis. AIAA SCITECH 2023 Forum, January, 1–18. https://doi.org/10.2514/6.2023-0373
Meddaikar, Y. M., Kier, T., Bartasevicius, J., Yu, F., Vanek, B., Olgyay, A., & Takarics, B. (2023). Aeroservoelastic induced drag modelling and minimization for the T-FLEX demonstrator. AIAA Scitech 2023 Forum, 1–20.
Yu, F., Bartasevicius, J., & Hornung, M. (2022). COMPARING POTENTIAL FLOW SOLVERS FOR AERODYNAMIC CHARACTERISTICS ESTIMATION OF THE T-FLEX UAV. International Council of the Aeronautical Sciences.
Wüstenhagen, M., Ackermann, L., & Bartasevicius, J. (2021). Validation and Update of an Aeroservoelastic Model based on Flight Test Data.
Sodja, J., De Breuker, R., Meddaikar, Y. M., Dillinger, J., Soal, K., Govers, Y., Krüger, W. R., Georgopoulos, P., Koimtzoglou, C., Roessler, C., Koeberle, S., Bartasevicius, J., Teubl, D., Gyulai, L., Tóth, S., Nagy, M., Balogh, D., Jásdi, M., Bauer, P., & Vanek, B. (2020). Ground testing of the flexop demonstrator aircraft. AIAA Scitech 2020 Forum, 1 PartF. https://doi.org/10.2514/6.2020-1968
Takarics, B., Patartics, B., Luspay, T., Bauer, P., Vanek, B., Rößler, C., Bartasevicius, J., Köberle, S., Teubl, D., Hornung, M., Waitman, S., Marcos, A., Pusch, M., Wüstenhagen, M., Kier, T., Looye, G., & Meddaikar, Y. M. (2020). Active flutter mitigation testing on the flexop demonstrator aircraft. AIAA Scitech 2020 Forum, 1 PartF, 1–29. https://doi.org/10.2514/6.2020-1970
Roessler, C., Bartasevicius, J., Koeberle, S. J., Teubl, D., Hornung, M., Meddaikar, Y. M., Dillinger, J. K. S., Krüger, W. R., Wüstenhagen, M., Ossmann, D., Kier, T., Looye, G., Sodja, J., Breuker, R., Luspay, T., Gyulai, L., Balogh, D., Vanek, B., Georgopoulos, P., & Koimtzoglou, C. (2020). Results of an aeroelastically tailored wing on the flexop demonstrator aircraft. AIAA Scitech 2020 Forum, 1 PartF. https://doi.org/10.2514/6.2020-1969
Roessler, C., Stahl, P., Sendner, F., Hermanutz, A., Koeberle, S., Bartasevicius, J., Rozov, V., Breitsamter, C., Hornung, M., Meddaikar, Y. M., Dillinger, J., Sodja, J., De Breuker, R., Koimtzoglou, C., Kotinis, D., & Georgopoulos, P. (2019). Aircraft Design and Testing of FLEXOP Unmanned Flying Demonstrator to Test Load Alleviation and Flutter Suppression of High Aspect Ratio Flexible Wings. AIAA Scitech 2019 Forum, 1–20. https://doi.org/10.2514/6.2019-1813
Buzica, A., Bartasevicius, J., & Breitsamter, C. (2017). Experimental investigation of high-incidence delta-wing flow control. Experiments in Fluids, 58(9). https://doi.org/10.1007/s00348-017-2408-9