Drone Projects

Showcasing UAV platforms I designed and developed, including flying-wing and fixed-wing systems, optimized for stability, efficiency, and autonomous control.

Flying Wing (Dec 2025 – Present)

Preliminary Design

Conceptualized a 1 kg flying-wing UAV with stability-focused geometry optimized for cruising at 30+ km/h. Incorporated MH60 root airfoil with PW51 wingtips, V-tail, and dihedral for strong aerodynamic stability.

Flying Wing Preliminary Design

CAD

Detailed CAD modeling in SolidWorks, integrating structural and avionics design with modular mounts for future FPV and payloads.

Flying Wing CAD

Analysis

Aerodynamic and stability analysis using XFLR5 and ANSYS, tuning washout, sweep, and dihedral to achieve optimal longitudinal and lateral damping.

Flying Wing Analysis
Flying Wing Final 1 Flying Wing Final 2 Flying Wing Final 3

Fixed-Wing Long-Range Platform V2 (Oct 2024 – Jan 2025)

Preliminary Design

Conceptualized a long-range fixed-wing UAV, designed for extended endurance. Airfoils were validated experimentally by using a homebuilt wind tunnel setup, shown on the right.

Fixed-Wing V2 Preliminary Design using Wind Tunnel

CAD

3D CAD modeling focused on structural layout and integration of avionics and payload, though the design could not be flown without a license.

Fixed-Wing V2 CAD
Fixed-Wing V2 Final 1 Fixed-Wing V2 Final 4
Fixed-Wing V2 Final 2 Fixed-Wing V2 Final 3

Fixed-Wing Long-Range Platform V1 (Nov 2023 – Feb 2024)

Preliminary Design

Initial fixed-wing concept with aerodynamic optimization for endurance, balancing wing area, airfoil selection, and tail configuration.

Fixed-Wing V1 Preliminary Design

CAD

CAD modeling of structural components and avionics layout, refining weight distribution and stability features for long-range flight.

Fixed-Wing V1 CAD
Fixed-Wing V1 Final 1 Fixed-Wing V1 Final 2 Fixed-Wing V1 Final 3