| Aeroservoelastic modeling and analysis of a highly flexible flutter demonstrator M Wuestenhagen, T Kier, YM Meddaikar, M Pusch, D Ossmann, ... 2018 atmospheric flight mechanics conference, 3150, 2018 | 52 | 2018 |
| Laminate optimization of blended composite structures using a modified Shepard’s method and stacking sequence tables YM Meddaikar, FX Irisarri, MM Abdalla Structural and Multidisciplinary Optimization 55 (2), 535-546, 2017 | 45 | 2017 |
| Aircraft Aeroservoelastic Modelling of the FLEXOP Unmanned Flying Demonstrator YM Meddaikar, J Dillinger, T Klimmek, W Krueger, M Wuestenhagen, ... AIAA Scitech 2019 Forum, 1815, 2019 | 42 | 2019 |
| 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 | 40 | 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 | 32 | 2020 |
| Static Aeroelastic Stiffness Optimization of a Forward Swept Composite Wing with CFD Corrected Aero Loads J Dillinger, MM Abdalla, YM Meddaikar, T Klimmek | 29* | 2015 |
| Loads and Structural Optimization Process for Composite Long Range Transport Aircraft Configuration KR Bramsiepe, V Handojo, YM Meddaikar, M Schulze, T Klimmek 2018 Multidisciplinary Analysis and Optimization Conference, 3572, 2018 | 27 | 2018 |
| Static and Dynamic Aeroelastic Validation of a Flexible Forward Swept Composite Wing M Ritter, J Dillinger, YM Meddaikar 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2017 | 27 | 2017 |
| 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 | 17 | 2020 |
| Lamination Parameters for Sandwich and Hybrid Material Composites GHC Silva, Y Meddaikar AIAA Journal 58 (10), 4604-4611, 2020 | 16 | 2020 |
| Design and Wind Tunnel Test of an Actively Controlled Flexible Wing WR Krüger, J Dillinger, Y Meddaikar, J Lübker, M Tang, W Meier, M Pusch, ... Proceedings of the International Forum on Aeroelasticity and Structural …, 2019 | 16 | 2019 |
| Optimization & testing of aeroelastically-tailored forward swept wings MY Meddaikar, J Dillinger, MR Ritter, Y Govers | 16 | 2017 |
| Optimization, Manufacturing and Testing of a Composite Wing with Maximized Tip Deflection YM Meddaikar, JK Dillinger, J Sodja, H Mai, R De Breuker 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2016 | 16 | 2016 |
| 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 | 15 | 2020 |
| Design and Optimization of an Aeroservoelastic Wind Tunnel Model JKS Dillinger, YM Meddaikar, J Lübker, M Pusch, T Kier Fluids 5 (1), 35, 2020 | 14 | 2020 |
| Application of Aeroelastic Tailoring for Load Alleviation on a Flying Demonstrator Wing WR Krüger, YM Meddaikar, JKS Dillinger, J Sodja, R De Breuker Aerospace 9 (10), 535, 2022 | 11 | 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 | 10 | 2023 |
| Blended composite optimization combining stacking sequence tables and a modified Shepard’s method MY Meddaikar, FX Irisarri, MM Abdalla | 10 | 2015 |
| Skin Panel Optimization of the Common Research Model Wing Using Sandwich Composites YM Meddaikar, JKS Dillinger, GHC Silva, R De Breuker Journal of Aircraft 59 (2), 386-399, 2021 | 9 | 2021 |
| TU-Flex: A Very-Flexible Flying Demonstrator with a Generic Transport Aircraft Configuration P Gonzalez, G Stavorinus, FJ Silvestre, A Voß, YM Meddaikar, W Krueger AIAA Scitech 2023 Forum, 1312, 2023 | 8 | 2023 |
Johannes DillingerDLR - Institute of AeroelasticityVerified email at dlr.de
