GrabCAD 模型信息
Fixed-Wing UAV Structural Airframe · 模型 97517
Overview Research-driven fixed-wing UAV developed and focused on achieving structural strength and reliable payload-carrying capability within compact dimensional constraints. Specifications Length: 42 in Wingspan: 64 in Airfoil: NACA 2412 (10 in chord) Fuselage Width: 4.5 in Design Focus The airframe was designed to balance structural rigidity and payload capacity while maintaining aerodynamic efficiency. The NACA 2412 airfoil was selected for its stable lift characteristics and suitability for low-speed flight conditions. Key Features Structural layout optimized for payload integration Compact fuselage design for efficient packaging and transport. Wing geometry designed for stable and predictable flight behavior. Outcome The project demonstrates system-level understanding of UAV airframe design, integrating aerodynamic selection, structural layout, and mission-driven constraints into a unified configuration. Blueprint https://grabcad.com/library/rc-plane-3 © Talha Qureshi
- 格式
- Rendering、SOLIDWORKS、STEP / IGES、Text file
- 分类
- Aviation、Educational、Tech
- 标签
- stp、step、solidworks、uav
- 数据更新
- 2026-10-13T16:45:31Z
