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Autonomous VTOL-Design & Analysis
Design configuration, aerodynamic and stability analysis of the Autonomous Y3 VTOL UAV designed for long-endurance fixed-wing flight. Designed to operate at a maximum take off mass of 5 kg and Its key
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Blended Wing VTOL Design
Blended Wing VTOL
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Early iteration of Fixed wing VTOL design
For final year project.
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at2308-tmotor-asm
Motor I made as a mock up for VTOL design
Designer
Carlos Sanchez
Aerospace Engineer | Aircraft Design | CATIA V5
Aerospace engineer and technical consultant with 10+ years of experience in the design, simulation, and development of manned and unmanned aircraft systems. I specialize in CAD surface modeling (CATIA
Designer
esade
Aircraft Engineer
concept to flying hardware: aerodynamic design, CFD, structural layout, CAD, composite manufacturing, and flight testing. I've designed and delivered fixed-wing, VTOL quadplane, WIG (wing-in-ground effect
Designer
ganta_yavan
Product Designer | VTOLs | Drones | EV Systems | Sustainable Innovation
🎯 Mechanical Design Engineer | UAVs | Robotics | CAD | Prototyping Expert I’m a mechanical design engineer with 5+ years of experience specializing in drones (UAVs, VTOLs), robotics, and electric mobility
3D Model
VTOL UAV DESIGN
VTOL UAV DESIGN FOR COMMERCIAL AND DEFENSE APPLICATION
Job
Hybrid VTOL drone design
CAD designer to create detailed designs for a hybrid VTOL (Vertical Take-Off and Landing) drone. The project involves innovative engineering and design considerations specific to hybrid technology. The ideal
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Tilt Rotor VTOL Vehicle
The main goal of the project is to design a simple solution to achieve hovering, vertical take-off, and landing capabilities for an airplane.