| Seit 2002 | Gruppenleiter, Institut für Flugzeugbau und Leichtbau, Technische Universität Braunschweig |
| 1996 - 2002 | Wissenschaftlicher Assistent, Institut für Flugzeugbau und Leichtbau |
| 1988 - 1996 | Wissenschaftlicher Mitarbeiter, Institut für Flugzeugbau und Leichtbau |
| 1996 | Promotion Dr.-Ing., Fakultät Maschinenbau der TU Braunschweig |
| 1988 | Diplom, Dipl.-Ing. Maschinenbau, TU Braunschwieg |
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., 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
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
Rohdenburg, M., Runge, F., Haupt, M., Markgraf, L., Horst, P., Heimbs, S.:Holistic Low-Effort Model for Damage Tolerance Analysis in Preliminary Design, 2022. Transactions on Aerospace Research 22, 1–20. doi.org/10.2478/tar-2022-0013
Talele, M., Haupt, M., Tooren, M. van, Elham, A.: Concurrent stringer topology and skin steered fiber pattern optimization for grid stiffened composite shell structures, 2021. Composite Structures 266, 113804. https://doi.org/10.1016/j.compstruct.2021.113804
Hötte, F., Sethe, C., Fiedler, T., Haupt, M., Haidn, O.J., Rohdenburg, M.: Experimental Lifetime Study of Regeneratively Cooled Rocket Chamber Walls, 2020. International Journal of Fatigue 105649.
Hötte, F., Haupt, M.C.:Transient 3D conjugate heat transfer simulation of a rectangular GOX–GCH4 rocket combustion chamber and validation, 2020. Aerospace Science and Technology 105, 106043.
Hötte, F.; Lungu, P.; von Sethe, C.; Fiedler, T.; Haupt, M.C.; Haidn, O.J.: Experimental Investigations of Thermomechanical Fluid-Structure Interaction in Rocket Combustion Chambers, AIAA Journal of Propulsion and Power, 35(5):906-916, 2019
Sommerwerk, K.; Michels, B.; Haupt, M.C.; Horst, P.: Influence of engine modeling on structural sizing and approach aerodynamics of a circulation controlled wing. CEAS Aeronautical Journal, 9(1):219-233, 2018
Sommerwerk, K.; Woidt, M.; Haupt, M.; Horst, P.: Reissner–Mindlin shell implementation and energy conserving isogeometric multi-patch coupling; International Journal for Numerical Methods in Engineering, 109(7):982–1012, 2017
Haupt, M.; Kowollik, D.; Lindhorst, K.; Hötte, F.: Fluid-Structure-Interaction in Rocket Thrust Chambers Simulation and Validation. Defect and Diffusion Forum, 366:97-117, 2016
Lindhorst, K.; Haupt, M.; Horst, P.: Reduced-order modelling of non-linear, transient aero-dynamics of the HIRENASD wing; Aeronautical Journal, 120(1226):601-626, 2016.
Lindhorst, K.; Haupt, M.C.; Horst, P.: Aeroelastic Analyses of the High-Reynolds-Number-Aerostructural-Dynamics Configuration Using a Nonlinear Surrogate Model Approach. AIAA Journal, 53(9):2784-2796, 2015
Lindhorst, K.; Haupt, M.C.; Horst, P.: Efficient Surrogate Modelling of Nonlinear Aerodynamics in Aerostructural Coupling Schemes. AIAA Journal, 52:1952-1966, 2014
Sommerwerk, K.; Haupt, M. C.: Design analysis and sizing of a circulation controlled CFRP wing with Coanda flaps via CFD-CSM coupling. CEAS Aeronautical Journal, 5(1):95-108, 2014
Kowollik, D.; Tini, V.; Reese, S.; Haupt, M.C.: 3D fluid-structure interaction analysis of a typical liquid rocket engine based on a novel viscoplastic damage model. International Journal for Numerical Methods in Engineering, 94:1165-1190, 2013
Möhle, E.; Haupt, M.C.; Horst, P.: Coupled Numerical Simulation and Experimental Validation of the Electro Impulse De-Icing Process. J. of Aircraft, 50:96-102, 2013
Unger, R.; Haupt, M.C.; Horst P.; Radespiel R.: Fluid-structure analysis of a flexible flapping airfoil at low Reynolds number flow. J. of Fluids and Structures, 28:72-88, 2012
Institut für Flugzeugbau und Leichtbau
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D-38108 Braunschweig
E-Mail: ifl@tu-braunschweig.de
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