| Design and sizing of a parametric structural model for a UCAV configuration for loads and aeroelastic analysis A Voss, T Klimmek CEAS Aeronautical Journal 8, 67-77, 2017 | 27 | 2017 |
| Preparation of Loads and Aeroelastic Analyses of a High Altitude, Long Endurance, Solar Electric Aircraft A Voß, V Handojo, C Weiser, S Niemann AEC2020 Aerospace Europe Conference, 2020 | 18 | 2020 |
| Aerodynamic and aeroelastic uncertainty quantification of NATO STO AVT-251 unmanned combat aerial vehicle A Da Ronch, J Drofelnik, MPC van Rooij, JC Kok, M Panzeri, A Voß Aerospace Science and Technology 91, 627-639, 2019 | 18 | 2019 |
| An Implementation of the Vortex Lattice and the Doublet Lattice Method A Voß https://elib.dlr.de/136536/, 2020 | 12 | 2020 |
| Open and closed loop gust loads analyses for a flying wing configuration with variable longitudinal stability A Voß Aerospace Science and Technology 89, 1-10, 2019 | 12 | 2019 |
| Maneuver loads calculation with enhanced aerodynamics for a UCAV configuration A Voss, T Klimmek AIAA Modeling and Simulation Technologies Conference, 2016 | 12 | 2016 |
| Results from loads and aeroelastic analyses of a high altitude, long endurance, solar electric aircraft A Voß, V Handojo, S Niemann, C Weiser Journal of Aeroelasticity and Structural Dynamics 8 (2), 2022 | 11 | 2022 |
| Design and sizing of an aeroelastic composite model for a flying wing configuration with maneuver, gust, and landing loads K Bramsiepe, A Voß, T Klimmek CEAS Aeronautical Journal, 1-15, 2020 | 11 | 2020 |
| Design and structural optimization of a flying wing of low aspect ratio based on flight loads A Voß Technische Universität Berlin, 2020 | 11 | 2020 |
| Structural Design Efforts for the MULDICON Configuration JM Schweiger, A Cunningham, E Sakarya, MJ Dalenbring, A Voß 2018 Applied Aerodynamics Conference, AIAA AVIATION Forum, 2018 | 10 | 2018 |
| Gust Loads Calculation of a Flying Wing Configuration A Voß 2018 Applied Aerodynamics Conference, AIAA AVIATION Forum, 2018 | 10 | 2018 |
| Design and sizing of an aeroelastic composite model for a UCAV configuration with maneuver, gust, and landing loads K Bramsiepe, A Voß, T Klimmek Deutscher Luft-und Raumfahrtkongress 2017, 2017 | 9 | 2017 |
| Loads Kernel User Guide A Voß https://elib.dlr.de/140268/, 2020 | 8 | 2020 |
| Dynamic maneuver loads calculations for a sailplane and comparison with flight test A Voß, P Ohme CEAS Aeronautical Journal 9 (3), 445-460, 2018 | 8 | 2018 |
| Dynamic aeroelastic stability analyses of parameterized flying wing configurations P Schreiber, C Vidy, A VOß, J Arnold, C Mack DLRK 2018-Proceedings, 2018 | 8 | 2018 |
| Flight mechanical design and analysis of a solar-powered high-altitude platform YJ Hasan, MS Roeser, M Hepperle, S Niemann, A Voß, V Handojo, ... | 5 | 2020 |
| Flight mechanical analysis of a solar-powered high-altitude platform YJ Hasan, MS Roeser, M Hepperle, S Niemann, A Voß, V Handojo, ... CEAS Aeronautical Journal 14 (1), 201-223, 2023 | 4 | 2023 |
| Aeroelastic Modeling, Loads Analysis and Structural Design of a Fighter Aircraft A Voß, T Klimmek | 4 | 2022 |
| Identifizierung dimensionierender Lastfälle auf Ebene finiter Elemente an einer Nurflügelstruktur im Vergleich zur Schnittlastmethode M Herberhold HAW Hamburg, 2020 | 4 | 2020 |
| Comparing VLM and CFD Maneuver Loads Calculations for a Flying Wing Configuration A Voß 18th International Forum on Aeroelasticity and Structural Dynamics, 2019 | 4 | 2019 |
