Aerostructural Design Manufacturing UAV Wings is a M.Tech project topic for Aerospace Engineering. It gives students a clear starting point for research, implementation planning, and documentation.
Aerostructural Design Manufacturing UAV Wings Project Details
| Abstract |
This systematic review examines the multidisciplinary optimization challenges of the design of wings for Unmanned Aerial Vehicles (UAVs). In particular, it focuses on the trade-offs between maximizing aerodynamic efficiency and minimizing the overall structure weight of high-aspect ratio wings (>15) used for long-endurance missions. This review critically examines 39 studies covering a 15-year span of integrated Computational Fluid Dynamics (CFD) and Finite Element Analysis (FEA) with advanced manufacturing to identify systematic deficiencies within the design-to-manufacturing process. One of the main findings is that the NACA 4412 airfoil is highly effective in low Reynolds number regimes, owing to its ability to mitigate the Laminar Separation Bubble (LSB), a phenomenon that can
increase drag by as much as 50%. The review also points out a significant modeling flaw; the rigid-wing assumption fails to properly consider the negative twist (washout) aeroelastic effect in flexible wings, producing a lift overestimate of roughly 7%. In addition, the study shows that Z-axis anisotropy in topology-optimized, additively manufactured structures can reduce structural performance by as much as 50%. This research illustrates the importance and need for aerostructural design integration considering aeroelasticity and manufacturing material properties to optimize the performance of UAV wings.
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| Reference Paper |
Aerostructural Design and Manufacturing of UAV Wings: A Systematic Review |
| Domain |
Aerospace Engineering |
| Sub-Domain |
Aerodynamics & Propulsion / Computational Aerodynamics / CFD for Aircraft |
| PDF Download |
Download / View PDF |
| Get Help |
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