24 results on '"Moschetta, Jean-Marc"'
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2. Development of a Hydrogen-powered UAV System for Crossing the Atlantic Ocean
3. Aerodynamic and Aeroacoustic Study of Low Reynolds Number Rotors: Influence of Pitch Angle, Airfoil Camber and Thickness
4. Flight Testing of Dynamic Soaring Part-2 : Open-Field Inclined Circle Trajectory
5. Flight Testing of Dynamic Soaring Part-1 : Leeward Inclined Circle Trajectory
6. Conceptual Design for Long-Endurance Convertible Unmanned Aerial System
7. Propulsive Performance for an Oscillating Airfoil Applied to Mini Air Vehicles
8. Experimental Analysis of a Blown-Wing Configuration during Transition Flight
9. Towards a Unified Model-Free Control Architecture for Tailsitter Micro Air Vehicles: Flight Simulation Analysis and Experimental Flights
10. Prediction of Noise from Low Reynolds Number Rotors with Different Number of Blades using a Non-Linear Vortex Lattice Method
11. Addendum: Aerodynamic Modeling of Propeller Forces and Moments at High Angle of Incidence
12. Regenerative Dynamic Soaring Trajectory Augmentation over Flat Terrains
13. Bioinspired Energy Harvesting from Atmospheric Phenomena for Small Unmanned Aerial Vehicles
14. Experimental Analysis of Propeller Forces and Moments at High Angle of Incidence
15. Aerodynamic Modeling of Propeller Forces and Moments at High Angle of Incidence
16. Flow Studies around a Small Propeller in Converting Maneuver
17. Performance Improvement of Small UAVs Through Energy-Harvesting Within Atmospheric Gusts
18. Aerothermodynamical Study for the Entry of an Apophis-Like Asteroid
19. Aerodynhamic Analysis of a Multi-Mission Short Shrouded Coaxial UAV: Part III - CFD for Hovering Flight
20. Aerodynamic Analysis of a Multi-Mission Short-Shrouded Coaxial UAV: Part II - Translation Flight
21. From Development of Micro Air Vehicle Testing Research to the Prototype of TYTO: Low Speed Biplane MAV
22. Aerodynamic Analysis of a Multi-Mission Short-Shrouded Coaxial UAV: part I-Hovering Flight
23. On Fixed-Wing Micro-Air Vehicles with Hovering Capabilities
24. Optimization of a Biplane Micro Air Vehicle
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