Designing aerodynamic devices for UAV – lessons learned
Comparison of different fidelity mass analyses
Guest editorial: 15th READ conference & 16th EWADE workshop
Impact of the aileron gap sealing on the aileron effectiveness
Mechanical aspects of mothership with sensing drones system
FDM 3D printing method utility assessment in small RC aircraft design
Stability analysis of the experimental airplane powered by a pulsejet engine
Partially feasible solution space for integrated SATS operations
MALE UAV design of an increased reliability level
MALE UAV design of an increased reliability level