Three surface aircraft (TSA) configuration – flying qualities evaluation
Stability analysis of the experimental airplane powered by a pulsejet engine
Partially feasible solution space for integrated SATS operations
Mechanical aspects of mothership with sensing drones system
MALE UAV design of an increased reliability level
MALE UAV design of an increased reliability level
Impact of the aileron gap sealing on the aileron effectiveness
Guest editorial: 15th READ conference & 16th EWADE workshop
Formulation of the optimization problem for engine mount design – tractor propeller case
FDM 3D printing method utility assessment in small RC aircraft design
Designing aerodynamic devices for UAV – lessons learned
Comparison of different fidelity mass analyses
Common computational model for coupling panel method with finite element method
Aerodynamic calculation of unmanned aircraft