Analysis and design of hybrid electric regional turboprop aircraft
The acceptance of civil drones in Germany
Business model options for passenger urban air mobility
Gust load alleviation for a long-range aircraft with and without anticipation
Reduced-order models for aerodynamic applications, loads and MDO
Modeling of aircraft fuel consumption using machine learning algorithms
Trajectory optimization in daily operations
About the emissions of alternative jet fuels
Outlook on ecologically improved composites for aviation interior and secondary structures
Ultra-high temperature ceramics developments for hypersonic applications
Impact of climate costs on airline network and trajectory optimization: a parametric study
Scale-resolving simulations using a lattice Boltzmann-based approach
Exploitation of hybrid anechoic wind tunnels for aeroacoustic and aerodynamic measurements
Aircraft trajectory optimization with dynamic input variables
Performance analysis of a hybrid-electric retrofit of a RUAG Dornier Do 228NG
SFB 880: fundamentals of high lift for future commercial aircraft
Investigation of the sooting propensity of aviation fuel mixtures
Investigation of the small-scale statistics of turbulence in the Modane S1MA wind tunnel
About the interaction between composition and performance of alternative jet fuels
CMDOWS: a proposed new standard to store and exchange MDO systems
Semi-analytical finite element method for modeling of lamb wave propagation
Free vibration studies on plates with central cut-out
Efficient continuous curvature path generation with pseudo-parametrized algebraic splines
A CFD benchmark of active flow control for buffet prevention
Sound quality assessment of a medium-range aircraft with enhanced fan-noise shielding design
Sensitivity and calibration of turbulence model in the presence of epistemic uncertainties
Central Reference Aircraft data System (CeRAS) for research community
Advanced low-noise aircraft configurations and their assessment: past, present, and future
Linearly variable chord-extension morphing for helicopter rotor blades
AAA process: a new approach to affordable fly-by-wire systems for CS23 aircraft
Aerodynamic angle estimation: comparison between numerical results and operative environment data
Improving GPS positioning accuracy using weighted Kalman Filter and variance estimation methods
Sizing of the energy storage system of hybrid-electric aircraft in general aviation