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Arne Voß
Arne Voß
German Aerospace Center (DLR), Institute of Aeroelasticity
Verified email at dlr.de
Title
Cited by
Cited by
Year
Design and sizing of a parametric structural model for a UCAV configuration for loads and aeroelastic analysis
A Voss, T Klimmek
CEAS Aeronautical Journal 8, 67-77, 2017
272017
Preparation of Loads and Aeroelastic Analyses of a High Altitude, Long Endurance, Solar Electric Aircraft
A Voß, V Handojo, C Weiser, S Niemann
AEC2020 Aerospace Europe Conference, 2020
212020
Aerodynamic and aeroelastic uncertainty quantification of NATO STO AVT-251 unmanned combat aerial vehicle
A Da Ronch, J Drofelnik, MPC van Rooij, JC Kok, M Panzeri, A Voß
Aerospace Science and Technology 91, 627-639, 2019
192019
An Implementation of the Vortex Lattice and the Doublet Lattice Method
A Voß
https://elib.dlr.de/136536/, 2020
182020
Results from loads and aeroelastic analyses of a high altitude, long endurance, solar electric aircraft
A Voß, V Handojo, S Niemann, C Weiser
Journal of Aeroelasticity and Structural Dynamics 8 (2), 2022
142022
Design and structural optimization of a flying wing of low aspect ratio based on flight loads
A Voß
Technische Universität Berlin, 2020
142020
Flight mechanical analysis of a solar-powered high-altitude platform
YJ Hasan, MS Roeser, M Hepperle, S Niemann, A Voß, V Handojo, ...
CEAS Aeronautical Journal 14 (1), 201-223, 2023
132023
Open and closed loop gust loads analyses for a flying wing configuration with variable longitudinal stability
A Voß
Aerospace Science and Technology 89, 1-10, 2019
132019
Parametric aeroelastic modeling, maneuver loads analysis using CFD methods and structural design of a fighter aircraft
A Voß, T Klimmek
Aerospace Science and Technology 136, 108231, 2023
122023
Loads Kernel User Guide
A Voß
https://elib.dlr.de/140268/, 2020
122020
Design and sizing of an aeroelastic composite model for a flying wing configuration with maneuver, gust, and landing loads
K Bramsiepe, A Voß, T Klimmek
CEAS Aeronautical Journal, 1-15, 2020
122020
Structural Design Efforts for the MULDICON Configuration
JM Schweiger, A Cunningham, E Sakarya, MJ Dalenbring, A Voß
2018 Applied Aerodynamics Conference, AIAA AVIATION Forum, 2018
122018
Maneuver loads calculation with enhanced aerodynamics for a UCAV configuration
A Voss, T Klimmek
AIAA Modeling and Simulation Technologies Conference, 2016
122016
Gust Loads Calculation of a Flying Wing Configuration
A Voß
2018 Applied Aerodynamics Conference, AIAA AVIATION Forum, 2018
102018
Design and sizing of an aeroelastic composite model for a UCAV configuration with maneuver, gust, and landing loads
K Bramsiepe, A Voß, T Klimmek
Deutscher Luft-und Raumfahrtkongress 2017, 2017
92017
Dynamic maneuver loads calculations for a sailplane and comparison with flight test
A Voß, P Ohme
CEAS Aeronautical Journal 9 (3), 445-460, 2018
82018
Dynamic aeroelastic stability analyses of parameterized flying wing configurations
P Schreiber, C Vidy, A VOß, J Arnold, C Mack
DLRK 2018-Proceedings, 2018
82018
TU-Flex: A Very-Flexible Flying Demonstrator with a Generic Transport Aircraft Configuration
P Gonzalez, G Stavorinus, FJ Silvestre, A Voß, YM Meddaikar, W Krueger
AIAA Scitech 2023 Forum, 1312, 2023
62023
Aeroelastic Modeling, Loads Analysis and Structural Design of a Fighter Aircraft
A Voß, T Klimmek
62022
Flight mechanical design and analysis of a solar-powered high-altitude platform
YJ Hasan, MS Roeser, M Hepperle, S Niemann, A Voß, V Handojo, ...
62020
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