| Decision tree-based machine learning to optimize the laminate stacking of composite cylinders for maximum buckling load and minimum imperfection sensitivity HNR Wagner, H Köke, S Dähne, S Niemann, C Hühne, R Khakimova Composite Structures 220, 45-63, 2019 | 76 | 2019 |
| Global aerostructural design optimization of more flexible wings for commercial aircraft TF Wunderlich, S Dähne, L Reimer, A Schuster Journal of Aircraft 58 (6), 1254-1271, 2021 | 28 | 2021 |
| Overview of collaborative multi-fidelity multidisciplinary design optimization activities in the DLR project VicToria S Goertz, M Abu-Zurayk, C Ilic, TF Wunderlich, S Keye, M Schulze, ... AIAA Aviation 2020 Forum, 3167, 2020 | 26 | 2020 |
| Multidisciplinary optimization of an NLF forward swept wing in combination with aeroelastic tailoring using CFRP: DLR contribution to the LuFo IV joint research project AeroStruct T Wunderlich, S Dähne, L Heinrich, L Reimer CEAS Aeronautical Journal 8, 673-690, 2017 | 23 | 2017 |
| Gradient based structural optimization of a stringer stiffened composite wing box with variable stringer orientation S Dähne, C Hühne Advances in Structural and Multidisciplinary Optimization: Proceedings of …, 2018 | 14 | 2018 |
| Structural optimization of composite wings in an automated multi-disciplinary environment T Bach, L Heinrich, S Dähne, C Hühne 14th AIAA Aviation Technology, Integration, and Operations Conference, 2295, 2014 | 14 | 2014 |
| Rapid transformation of lamination parameters into stacking sequences M Sprengholz, H Traub, M Sinapius, S Dähne, C Hühne Composite Structures 276, 114514, 2021 | 10 | 2021 |
| Steps to feasibility for laminar wing design in a multidisciplinary environment S Dähne, T Bach, C Hühne | 10 | 2014 |
| Global aero-structural design optimization of composite wings with active manoeuvre load alleviation TF Wunderlich, S Dähne, L Reimer, A Schuster CEAS Aeronautical Journal 13 (3), 639-662, 2022 | 8 | 2022 |
| Aeroelastic tailoring of an NLF forward swept wing: DLR contribution to LuFo IV joint research project AeroStruct T Wunderlich, S Dähne CEAS Aeronautical Journal 8 (3), 461-479, 2017 | 8 | 2017 |
| Automated sizing of a composite wing for the usage within a multidisciplinary design process T Bach, T Führer, C Willberg, S Dähne Aircraft Engineering and Aerospace Technology: An International Journal 88 …, 2016 | 8 | 2016 |
| Design rules consideration within optimization of composite structures using lamination parameters E Werthen, S Dähne | 7 | 2016 |
| High-Fidelity-based MDO: A Closer Look at the Selected Sub-Processes Overall Aircraft Design Synthesis, Loads Analysis, and Structural Optimization T Klimmek, S Dähne, B Fröhler, J Hartmann, D Kohlgrüber, M Petsch, ... | 6 | 2020 |
| Design-and Manufacturing Constraints witin the Gradient Based Optimization of a Composite Aircraft Wingbox E Werthen, S Dähne 6th Airframe Struct. Des. Conf., no, 2018 | 5 | 2018 |
| Efficient gradient based optimization approach of composite stiffened panels in multidisciplinary environment S Dähne, C Hühne 5th Aircraft Structure Design Conference, 2016 | 5 | 2016 |
| Overview of collaborative high performance computing-based MDO of transport aircraft in the DLR project VicToria T Wunderlich, M Abu-Zurayk, C Ilic, J Jepsen, M Schulze, M Leitner, ... | 4 | 2018 |
| Structural concepts for passive load alleviation KR Bramsiepe, M Gröhlich, S Dähne, D Hahn AIAA Scitech 2022 Forum, 0687, 2022 | 3 | 2022 |
| Preliminary Design of Composite Wings using Beam-based Structural Models D Zerbst, T Hecken, P Balack, S Freund, E Werthen, S Dähne, C Hühne | 2 | 2022 |
| Damage tolerance allowable calculation for the aircraft design with static ultimate load R Bogenfeld, S Freund, S Dähne, T Wunderlich, T Wille Composite Structures 329, 117803, 2024 | 1 | 2024 |
| Gradient-based Design Optimization of Composite Structures using Double-Double Laminates D Zerbst, L Tönjes, C Ückert, S Dähne, E Werthen, E Kappel, C Hühne | 1 | 2023 |
