Daniel Hahn, M. Sc.

Wissenschaftlicher Mitarbeiter | Multidisziplinäre Design- und Simulationsmethoden

Kontakt

Raum 25

+49 531 391 9924

daniel.hahn(at)tu-braunschweig.de

Berufserfahrung

Seit 2019

Wissenschaftlicher Mitarbeiter, Institut für Flugzeugbau und Leichtbau, Technische Universität Braunschweig

Ausbildung

2017 - 2019	Master Luft- und Raumfahrttechnik, TU Braunschweig
2013 - 2017	Bachelor Maschinenbau, TU Braunschweig

Expertise

Fluid-Struktur-Interaktion
Finite-Elemente-Methode
Strömungssimulation
Lastabminderung

Projekte

SE²A B2.4 HyCoNoS| Sustainable and energy efficient aviation, Teilprojekt B2.4: Hybrid load alleviation by fluidic/reversed control and nonlinear structures

SKAiB| Skalierbare Brennstoffzellensysteme für elektrische Antriebe - oberflächenbasierter Wärmetauscher

SE²A B2.4 (2019)| Sustainable and energy efficient aviation, Teilprojekt B2.4: Morphing structures for the 1g-wing (abgeschlossen)

Veröffentlichungen

Kreuzeberg, L., Haupt, M., Hahn, D., Antonau, I., Heimbs, S.: Performance and Stability Assessment of a Coupled Three-Field Thermal Fluid-Structure Interaction Simulation of a Simplified Thin-Walled Skin Heat Exchanger, Presented at the 9th European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS2024, Lisbon, Portugal, 2024, https://www.scipedia.com/public/Kreuzeberg_et_al_2024a

Hahn, D., Haupt, M., Lobitz, L., Heimbs, S.,. Analysis of the structural behavior of wings with nonlinear components for passive load reduction, 2023. Presented at the Aerospace Europe Conference 2023 (Joint 10th EUCASS & 9th CEAS Conference), Lausanne, Switzerland.

Thel, S., Hahn, D., Haupt, M., Heimbs, S.,. A passive load alleviation aircraft wing: topology optimization for maximizing nonlinear bending–torsion coupling, 2022. Struct Multidisc Optim 65, 155. https://doi.org/10.1007/s00158-022-03248-3

Hahn, D., Khalil, K., Haupt, M., Bauknecht, A., Heimbs, S.,. Exploration of the synergies between fluidic flow control and nonlinear structural behavior for gust load alleviation, 2022, Presented at the Deutscher Luft-Und Raumfahrtkongress 2022, Dresden.

Hahn, D., Haupt, M., Heimbs, S.,. Load alleviation capabilities of wings with nonlinear structural behavior in stationary and dynamic load cases, 2022. Presented at the International Forum on Aeroelasticity and Structural Dynamics, Madrid, Spain.

Hahn, D., Haupt, M., Heimbs, S.,. Passive Load Alleviation by Nonlinear Stiffness of Airfoil Structures, 2022, in: AIAA SCITECH 2022 Forum. Presented at the AIAA SCITECH 2022 Forum, American Institute of Aeronautics and Astronautics, San Diego, CA & Virtual. https://doi.org/10.2514/6.2022-0318

Bramsiepe, K.R., Gröhlich, M., Dähne, S., Hahn, D.,. Structural Concepts for Passive Load Alleviation, 2022, in: AIAA SCITECH 2022 Forum. Presented at the AIAA SCITECH 2022 Forum, American Institute of Aeronautics and Astronautics, San Diego, CA & Virtual. https://doi.org/10.2514/6.2022-0687

Hahn, D., Haupt, M.,. Exploration of the effect of wing component post-buckling on bending-twist coupling for nonlinear wing twist, 2022. CEAS Aeronaut J. https://doi.org/10.1007/s13272-022-00586-2

Hahn, D., Haupt, M.,. Passive Load Alleviation by Nonlinear Mounting of Airfoils in 2-DOF Models, 2021, Presented at Deutscher Luft- und Raumfahrtkongress 2021, online. https://doi.org/10.25967/550238

Hahn, D., Haupt, M.,. Potential of the nonlinear structural behavior of wing design components for passive load alleviation, 2020, Presented at Deutscher Luft- und Raumfahrtkongress 2020, online