Robust High-Fidelity Dataset-Based Shape Optimization for Aircraft Design
Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.
2025
Hybrid Rotor Noise Optimization
94
The 14th EASN International Conference on “Innovation in Aviation & Space Towards Sustainability Today & Tomorrow”
Multidisciplinary Digital Publishing Institute (MDPI)
2025
Deep Learning Framework for Predicting Transonic Wing Buffet Loads Due to Structural Eigenmode-Based Deformations
Aerospace
2025
12
5
415
Rotor Wake Tail Interactions of a Helicopter Wind Tunnel Model with Various Rotor Head Configurations
European Rotorcraft Forum, Marseille, France, September 2024
2024
Flow Field Analysis on a Helicopter Wind Tunnel Model with Varying Blade Stub Lengths
Proceedings der 30. GALA-Fachtagung "Experimentelle Strömungsme- chanik", Munich, Germany 2023
German Association for Laser Anemometry GALA e.V., Karlsruhe, Germany,
2023
Nonlinear Folding Wing Tips for Gust Loads Alleviation
Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.
2024
Flow field analysis of a high agility type aircraft aeroelastic wind tunnel model
Aerospace Science and Technology
2025
162
110177
Design and investigation of an aeroelastically scaled delta-wing wind tunnel model for dynamic load analysis
CEAS Aeronautical Journal
2024
Volume 16
pages 275–291, (2025)
On-site aerodynamics using stereoscopic PIV and deep optical flow learning
Experiments in Fluids
2024
65
12
AERODYNAMIC INTERACTION EFFECTS OF TILTROTOR EVTOL AIRCRAFT
34th Congress of the International Council of the Aeronautical Sciences, ICAS 2024
International Council of the Aeronautical Sciences
2024