| Turbulence models in CFD J Sodja University of Ljubljana, 1-18, 2007 | 125 | 2007 |
| Design and testing of a low subsonic wind tunnel gust generator PMGJ Lancelot, J Sodja, NPM Werter, R De Breuker Advances in aircraft and spacecraft science 4 (2), 125, 2017 | 97 | 2017 |
| 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 |
| Design and experiments of a warp induced camber and twist morphing leading and trailing edge device N Werter, J Sodja, G Spirlet, R De Breuker 24th AIAA/AHS adaptive structures conference, 0315, 2016 | 34 | 2016 |
| Design of flexible propellers with optimized load-distribution characteristics J Sodja, R Drazumeric, T Kosel, P Marzocca Journal of Aircraft 51 (1), 117-128, 2014 | 31 | 2014 |
| Design and testing of aeroelastically tailored composite wing under fatigue and gust loading including effect of fatigue on aeroelastic performance D Rajpal, FMA Mitrotta, CA Socci, J Sodja, C Kassapoglou, R De Breuker Composite Structures 275, 114373, 2021 | 30 | 2021 |
| Computational fluid dynamics analysis of an optimized load-distribution propeller J Sodja, D Stadler, T Kosel Journal of aircraft 49 (3), 955-961, 2012 | 30 | 2012 |
| Experimental evaluation of the morphing leading edge concept J Sodja, MJ Martinez, JC Simpson, R De Breuker 23rd AIAA/AHS Adaptive Structures Conference, 0791, 2015 | 27 | 2015 |
| Experimental characterisation of flutter and divergence of 2D wing section with stabilised response J Sodja, F Roizner, R De Breuker, M Karpel Aerospace Science and Technology 78, 542-552, 2018 | 26 | 2018 |
| Assessment of low-fidelity fluid–structure interaction model for flexible propeller blades J Sodja, R De Breuker, D Nozak, R Drazumeric, P Marzocca Aerospace Science and Technology 78, 71-88, 2018 | 24 | 2018 |
| Morphing wing design using integrated and distributed trailing edge morphing T Mkhoyan, NR Thakrar, R De Breuker, J Sodja Smart Materials and Structures 31 (12), 125025, 2022 | 23 | 2022 |
| Design and Development of a Seamless Smart Morphing Wing Using Distributed Trailing Edge Camber Morphing for Active Control T Mkhoyan, NR Thakrar, R De Breuker, J Sodja AIAA Scitech 2021 Forum, 0477, 2021 | 20 | 2021 |
| Design of a smart morphing wing using integrated and distributed trailing edge camber morphing T Mkhoyan, NR Thakrar, R De Breuker, J Sodja Smart Materials, Adaptive Structures and Intelligent Systems 84027, V001T04A023, 2020 | 20 | 2020 |
| Experimental evaluation of a morphing leading edge concept J Sodja, MJ Martinez, JC Simpson, R De Breuker Journal of Intelligent Material Systems and Structures 30 (18-19), 2953-2969, 2019 | 18 | 2019 |
| Wing Stiffness and Hinge Release Threshold Effects on Folding Wingtip Gust Load Alleviation X Carrillo, C Mertens, A Sciacchitano, B van Oudheusden, R De Breuker, ... AIAA SCITECH 2022 Forum, 1559, 2022 | 17 | 2022 |
| 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 |
| 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 |
| Overview of the SmartX wing technology integrator R De Breuker, T Mkhoyan, N Nazeer, V Stuber, X Wang, I Mkhoyan, ... Actuators 11 (10), 302, 2022 | 15 | 2022 |
| Incremental Nonlinear Control For Aeroelastic Wing Load Alleviation and Flutter Suppression RRM Schildkamp, J Chang, J Sodja, R De Breuker, X Wang International Forum on Aeroelasticity and Structural Dynamics, 2022 | 15 | 2022 |
| 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 |
