- CFD-based Aeroelastic Sensitivity Study of a Configuration with a Very Flexible High-Aspect-Ratio Swept Wing. Aerospace 6, 2019 mehr…
- INFLUENCE ON THE FLUTTER BEHAVIOR OF PRE-STRESSED WING STRUCTURES UNDER AERODYNAMIC LOADING. IFASD 2019, 2019The International Forum on Aeroelasticity and Structural Dynamics mehr…
- Aeroservoelastic Modeling and Analysis of a Highly Flexible Flutter Demonstrator. American Institute of Aeronautics and Astronautics, 2018 mehr…
- Virtual Aaircraft Model for Aeroelastic Simulation and Load Prediction of a High-Aspect Ratio Composite Swept Wing. International Council of the Aeronautical Sciences, 2018 mehr…
- Feasibility Analysis and Comparative Assessment of Structural Power Technology in All-Electric Composite Aircraft. 67. Deutscher Luft- und Raumfahrtkongress, 2018 mehr…
- Mission and Aircraft Design of FLEXOP Unmanned Flying Demonstrator to Test Flutter Suppression within Visual Line of Sight. AIAA Aviation 2017, 2017 mehr…
Andreas Hermanutz, Dr.-Ing.
Technische Universität München
Lehrstuhl für Luftfahrtsysteme (Prof. Hornung)
Postadresse
Boltzmannstr. 15
85748 Garching b. München
- Tel.:
- andreas.hermanutz@tum.de
Forschungsbereich | Flugzeugentwurf |
Interessensschwerpunkt | Aeroelastik |
Projekte | VitAM - Flex |
Veröffentlichungen
- Mission and Aircraft Design of FLEXOP Unmanned Flying Demonstrator to Test Flutter Suppression within Visual Line of Sight. AIAA Aviation Forum, 2017 mehr…
- Aeroelastic Analysis of a Flutter Demonstrator with a Very Flexible High-Aspect-Ratio Swept Wing. IFASD [International Forum on Aeroelasticity and Structural Dynamics], 2017 mehr…
- 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 mehr…
- Multi-criteria optimization of an aircraft propeller considering manufacturing. Structural and Multidisciplinary Optimization, 2016 mehr…
- Shape Adaptive Technology for Aircraft Engine Nacelle Inlets. Aircraft Structural Design Conference [5th.], 2016 mehr…
- Technology Investigation of Morphing Inlet Lip Concepts for Flight Propulsion Nacelles. EUCASS [6., 2015, Krakau], 2015 mehr…
- A Morphing Lip Concept for Shape Variable Aircraft Engine Nacelles. DGLR Jahrestagung, 2015 mehr…
- Progress Towards Adaptive Aircraft Engine Nacelles. 29th Congress of the International Council of the Aeronautical Sciences, 2014 mehr…
- Formvariable Steuerflächen und deren aeroelastisches Verhalten am Beispiel des Sagitta Demonstrators. Deutscher Luft- und Raumfahrtkongress, 2012 mehr…