Author: Thiart, G. D.
Similar Items: Aerodynamic characteristics of a mission-adaptive stealthy air inlet
- Development and validation of a fixed wing UAV design model
- Trajectory planning methods applied to a rotary wing UAV with uncertain suspended payloads
- The performance of axial fans subjected to forced cross-flow at inlet
- Stall prevention control of fixed-wing unmanned aerial vehicles
- The effect of the boundary layer present in wind tunnels on the aerodynamic drag of a model truck
- Modelling a fuel cell propulsion system for multicopters