Παρακολούθηση
Julius Bartasevicius
Julius Bartasevicius
Η διεύθυνση ηλεκτρονικού ταχυδρομείου έχει επαληθευτεί στον τομέα tum.de
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Παρατίθεται από
Παρατίθεται από
Έτος
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
392019
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
302020
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
152020
Experimental investigation of high-incidence delta-wing flow control
A Buzica, J Bartasevicius, C Breitsamter
Experiments in Fluids 58 (9), 131, 2017
152017
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
142020
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
92021
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
82023
Comparing potential flow solvers for aerodynamic characteristics estimation of the T-Flex UAV
F Yu, J Bartasevicius, M Hornung
ICAS, 2022
72022
Discrete vortices on delta wings with unsteady leading-edge blowing
J Bartasevicius, A Buzica, C Breitsamter
8th AIAA Flow Control Conference, 3170, 2016
62016
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
42023
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
32022
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
32016
Lessons Learned from Flight Testing Active Flutter Suppression Technologies
J Bartasevicius, D Teubl, T Seren, F Yu, M Hornung, B Vanek, D Balogh, ...
12024
Aeroservoelastic Models for Design, Testing, Flight Test Clearance and Validation of Active Flutter Suppression Control Laws
T Kier, M Wüstenhagen, O Süelözgen, R Konatala, Y Meddaikar, K Soal, ...
International Forum on Aeroelasticity and Structural Dynamics IFASD, 2024
12024
In-flight drag measurement and validation for a medium-sized UAV
J Bartasevicius, M Hornung
AIAA SCITECH 2023 Forum, 0372, 2023
12023
Flutter flight testing: Using operational modal analysis to identify, track and predict flutter for safe and efficient flight test campaigns
KI Soal, J Schwochow, R Volkmar, M Tang, C Thiem, Y Govers, ...
2024
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, M Tang, P Lubrina, R Volkmar, Y Govers, ...
2024
D3. 2 Flight Test Report Phase
J Bartasevicius
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