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Technical University of Munich
Picture of Andreas Hermanutz

Andreas Hermanutz, Dr.-Ing.

Technical University of Munich

Chair of Aircraft Design (Prof. Hornung)

Postal address

Boltzmannstr. 15
85748 Garching b. München

Research AreaAircraft Design
Focus of InterestAeroelastics
ProjectsVitAM - Flex

Publications

  • Vladyslav Rozov, Andreas Volmering, Andreas Hermanutz, Mirko Hornung,Christian Breitsamter: CFD-based Aeroelastic Sensitivity Study of a Configuration with a Very Flexible High-Aspect-Ratio Swept Wing. Aerospace 6, 2019 more…
  • Andreas Hermanutz, Mirko Hornung: INFLUENCE ON THE FLUTTER BEHAVIOR OF PRE-STRESSED WING STRUCTURES UNDER AERODYNAMIC LOADING. IFASD 2019, 2019The International Forum on Aeroelasticity and Structural Dynamics more…
  • Matthias Wuestenhagen, Thiemo Kier, Manuel Pusch, Daniel Ossmann, Muhammad Yasser Meddaikar, Andreas Hermanutz: Aeroservoelastic Modeling and Analysis of a Highly Flexible Flutter Demonstrator. American Institute of Aeronautics and Astronautics, 2018 more…
  • Andreas Hermanutz, Mirko Hornung: Virtual Aaircraft Model for Aeroelastic Simulation and Load Prediction of a High-Aspect Ratio Composite Swept Wing. International Council of the Aeronautical Sciences, 2018 more…
  • Scholz, Anna Elena; Hermanutz, Andreas; Hornung, Mirko: Feasibility Analysis and Comparative Assessment of Structural Power Technology in All-Electric Composite Aircraft. 67. Deutscher Luft- und Raumfahrtkongress, 2018 more…
  • Stahl, Philipp; Sendner, Franz-Michael; Hermanutz, Andreas; Rößler, Christian; Hornung, Mirko: Mission and Aircraft Design of FLEXOP Unmanned Flying Demonstrator to Test Flutter Suppression within Visual Line of Sight. AIAA Aviation 2017, 2017 more…
  • Stahl, P.; Sendner, F.- M.; Rößler, C.; Hornung, M.; Hermanutz, A.: Mission and Aircraft Design of FLEXOP Unmanned Flying Demonstrator to Test Flutter Suppression within Visual Line of Sight. AIAA Aviation Forum, 2017 more…
  • Rozov, V.; Hermanutz, A.; Breitsamter, C.; Hornung, M.: Aeroelastic Analysis of a Flutter Demonstrator with a Very Flexible High-Aspect-Ratio Swept Wing. IFASD [International Forum on Aeroelasticity and Structural Dynamics], 2017 more…
  • Hermanutz, A.; Hornung, M.: High Fidelity Trim Calculation Under Consideration Of Aeroelastic Effects Of A High Aspect Ratio Swept Wing. IFASD [International Forum on Aeroelasticity and Structural Dynamics], 2017 more…
  • Schatz, Markus E.; Hermanutz, Andreas; Baier, Horst J.: Multi-criteria optimization of an aircraft propeller considering manufacturing. Structural and Multidisciplinary Optimization, 2016 more…
  • Kling, U.; Seitz, A.; Bijewitz, J.; Hermanutz, A.; da Rocha-Schmidt, L.; Scarpa, F.; Majic, F.; Efraimsson, G.; O´Reilly, C.J.: Shape Adaptive Technology for Aircraft Engine Nacelle Inlets. Aircraft Structural Design Conference [5th.], 2016 more…
  • Hermanutz, A.; Da Rocha-Schmidt, L.; Baier, H.: Technology Investigation of Morphing Inlet Lip Concepts for Flight Propulsion Nacelles. EUCASS [6., 2015, Krakau], 2015 more…
  • Da Rocha-Schmidt, Luiz; Hermanutz, A.; Baier, H.: A Morphing Lip Concept for Shape Variable Aircraft Engine Nacelles. DGLR Jahrestagung, 2015 more…
  • da Rocha-Schmidt, L.; Hermanutz, A.; Baier, H.; Seitz, A.; Bijewitz, J.; Isikveren, A. T.; Scarpa3, F.; Allegri, G.; Remillat, C.; Feuilloley, E.; Majic, F.; O’Reilly, C.; Efraimsson, G.: Progress Towards Adaptive Aircraft Engine Nacelles. 29th Congress of the International Council of the Aeronautical Sciences, 2014 more…
  • da Rocha-Schmidt, L.; Hermanutz, A.; Hofheinz, N.; Baier, H.: Formvariable Steuerflächen und deren aeroelastisches Verhalten am Beispiel des Sagitta Demonstrators. Deutscher Luft- und Raumfahrtkongress, 2012 more…
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