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
Author: Thiart, G. D.
- A discrete vortex model for the calculation of aerodynamic loads on a blade of a N-bladed helicopter rotor in rectilinear flight
- A numerical investigation into the heave, sway and roll motions of typical ship like hull sections using RANS numerical methods
- Development of a perturbation potential panel method for analysing rotating 3D bodies
- Aerodynamic characteristics of a mission-adaptive stealthy air inlet
- A numerical procedure for predicting the effects of distorted inflow conditions on the performance of axial flow fans
- Modelling of internal combustion engine intake and exhaust processes