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Johannes Achleitner
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Citata da
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Airfoil optimization with CST-parameterization for (un-) conventional demands
J Achleitner, K Rohde-Brandenburger, M Hornung
XXXIV Ostiv Congress, 117-120, 2018
192018
Multiresolution topology optimization of large-deformation path-generation compliant mechanisms with stress constraints
J Reinisch, E Wehrle, J Achleitner
Applied Sciences 11 (6), 2479, 2021
172021
Aerodynamic design of a morphing wing sailplane
J Achleitner, K Rohde-Brandenburger, P Rogalla von Bieberstein, ...
AIAA Aviation 2019 Forum, 2816, 2019
172019
Flexible multibody dynamics and sensitivity analysis in the design of a morphing leading edge for high-performance sailplanes
V Gufler, EJ Wehrle, J Achleitner, R Vidoni
Proceedings of the 10th ECCOMAS Thematic Conference on MULTIBODY DYNAMICS …, 2021
122021
Studies of anisotropic wing shell concepts for a sailplane with a morphing forward wing section
F Sturm, J Achleitner, K Jocham, M Hornung
AIAA Aviation 2019 Forum, 2817, 2019
122019
On material selection for topology optimized compliant mechanisms
J Achleitner, E Wehrle
Mechanism and Machine Theory 167, 104474, 2022
112022
A semi-analytical approach to sensitivity analysis with flexible multibody dynamics of a morphing forward wing section
V Gufler, E Wehrle, J Achleitner, R Vidoni
Multibody System Dynamics 58 (1), 1-20, 2023
92023
Highly extensible skin of a variable geometry wing leading edge of a high-performance sailplane
M Weinzierl, J Achleitner, HH Baier
Technical Soaring 39 (1), 4-9, 2015
72015
CellSkin-a new flexible shell structure for a morphing wing aircraft
J Achleitner, H Baier
International Conference on Composite Structures (19th, Porto, 2016), 2016
62016
Experimental study of flexible skin designs between a moving wing segment and a fixed wing part on a full scale demonstrator
M Radestock, J Riemenschneider, A Falken, J Achleitner
Smart Materials, Adaptive Structures and Intelligent Systems 84027, V001T03A008, 2020
42020
Hybrid-matrix composites: materials and manufacturing
J Krollmann, S Neuchl, PM Schaefer, J Achleitner, K Drechsler
SAMPE 2017-Society of the Advancement Material and Process Engineering, 2017
12017
FlexMat-TUM-Konzeptdefinition und Voruntersuchungen zu formvariablen Werkstoffen und Flugzeugkomponenten: Schlussbericht für den Berichtszeitraum 01.01. 2016 bis 31.03. 2019
K Heller, J Achleitner, K Drechsler
Technische Universität München, 2020
2020
Optimale Synthese nachgiebiger Mechanismen für die Robotik
EJ Wehrle, J Achleitner, J Reinisch
Universität Duisburg-Essen, 2019
2019
Experimental investigation of a hybrid skin design between de morphing leading edge and a fixed wing on a full scale demonstrator
J Riemenschneider, M Radestock, A Falken, J Achleitner
2019
Verbundvorhaben: In-Orbit Verifikation hochstabiler Bauweisen für Ka-Band Reflektoren und Antennen (H2KAR): Abschlussbericht: Abschlußdatum: 31.03. 2018
J Achleitner, M Hornung, H Baier
Technische Universität München, 2018
2018
Numerische Optimierung am Beispiel formvariabler Flügelstrukturen
J Achleitner, K Rohde-Brandenburger, J Reinisch, M Hornung
Seminarreihe Hochleistungsstrukturen im Leichtbau, 2018
2018
Forschungsaktivitäten im Bereich formvariabler Segelflugzeugflügel an der TU München
J Achleitner, K Rohde-Brandenburger, J Reinisch, M Hornung
Symposium für Segelflugzeugentwicklung, 2017
2017
ROBUST DESIGN OF A MORPHING AIRCRAFT WING
J Achleitner, K Rohde-Brandenburger, M Hornung, M Zimmermann
Il sistema al momento non può eseguire l'operazione. Riprova più tardi.
Articoli 1–18