Winglet Design for Aerodynamic and Performance Optimization of UAVs via Surrogate Modeling
The aerodynamic performance of an aircraft can be significantly enhanced by incorporating wingtip devices, such as winglets, which primarily reduce lift-induced drag caused by wingtip vortices. This study introduces a comprehensive optimization framework for designing winglets on a Class I fixed-win...
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MDPI AG
2025-01-01
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| Series: | Aerospace |
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| Online Access: | https://www.mdpi.com/2226-4310/12/1/36 |
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| author | Eleftherios Nikolaou Spyridon Kilimtzidis Vassilis Kostopoulos |
| author_facet | Eleftherios Nikolaou Spyridon Kilimtzidis Vassilis Kostopoulos |
| author_sort | Eleftherios Nikolaou |
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| description | The aerodynamic performance of an aircraft can be significantly enhanced by incorporating wingtip devices, such as winglets, which primarily reduce lift-induced drag caused by wingtip vortices. This study introduces a comprehensive optimization framework for designing winglets on a Class I fixed-wing mini-UAV, aiming to maximize aerodynamic efficiency and operational performance. Using surrogate-based optimization (SBO) techniques, this research developed winglet geometries with varying geometric parameters such as length, cant angle, and sweep angle with their performance being evaluated through high-fidelity Computational Fluid Dynamics (CFD) simulations. These simulations utilized Reynolds-Averaged Navier–Stokes (RANS) equations coupled with the Spalart–Allmaras turbulence model to capture the intricate flow dynamics around the UAV in different flight phases. The integration of SBO techniques allowed for an efficient exploration of the design space while reducing computational costs associated with iterative high-fidelity simulations. In particular, the proposed SBO framework optimized the UAV’s aerodynamic characteristics, including lift-to-drag ratio and drag reduction, followed by a stability and control analyses to ensure balanced performance for the optimal configurations. Dynamic stability evaluations revealed improved flight characteristics, maintaining control across operational envelopes. The results demonstrated a significant improvement in aerodynamic coefficients, range, endurance, and reduction in battery consumption throughout the entire UAV operational envelope, underscoring the potential of innovative winglet designs to enhance UAV performance across diverse mission profiles. |
| format | Article |
| id | doaj-art-9331920b25444d63850651df704e1275 |
| institution | Kabale University |
| issn | 2226-4310 |
| language | English |
| publishDate | 2025-01-01 |
| publisher | MDPI AG |
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| series | Aerospace |
| spelling | doaj-art-9331920b25444d63850651df704e12752025-01-24T13:15:33ZengMDPI AGAerospace2226-43102025-01-011213610.3390/aerospace12010036Winglet Design for Aerodynamic and Performance Optimization of UAVs via Surrogate ModelingEleftherios Nikolaou0Spyridon Kilimtzidis1Vassilis Kostopoulos2Applied Mechanics Laboratory, Mechanical Engineering and Aeronautics Department, University of Patras, Rio Campus, 26500 Patras, GreeceApplied Mechanics Laboratory, Mechanical Engineering and Aeronautics Department, University of Patras, Rio Campus, 26500 Patras, GreeceApplied Mechanics Laboratory, Mechanical Engineering and Aeronautics Department, University of Patras, Rio Campus, 26500 Patras, GreeceThe aerodynamic performance of an aircraft can be significantly enhanced by incorporating wingtip devices, such as winglets, which primarily reduce lift-induced drag caused by wingtip vortices. This study introduces a comprehensive optimization framework for designing winglets on a Class I fixed-wing mini-UAV, aiming to maximize aerodynamic efficiency and operational performance. Using surrogate-based optimization (SBO) techniques, this research developed winglet geometries with varying geometric parameters such as length, cant angle, and sweep angle with their performance being evaluated through high-fidelity Computational Fluid Dynamics (CFD) simulations. These simulations utilized Reynolds-Averaged Navier–Stokes (RANS) equations coupled with the Spalart–Allmaras turbulence model to capture the intricate flow dynamics around the UAV in different flight phases. The integration of SBO techniques allowed for an efficient exploration of the design space while reducing computational costs associated with iterative high-fidelity simulations. In particular, the proposed SBO framework optimized the UAV’s aerodynamic characteristics, including lift-to-drag ratio and drag reduction, followed by a stability and control analyses to ensure balanced performance for the optimal configurations. Dynamic stability evaluations revealed improved flight characteristics, maintaining control across operational envelopes. The results demonstrated a significant improvement in aerodynamic coefficients, range, endurance, and reduction in battery consumption throughout the entire UAV operational envelope, underscoring the potential of innovative winglet designs to enhance UAV performance across diverse mission profiles.https://www.mdpi.com/2226-4310/12/1/36unmanned air vehicle (UAV)fixed-wing UAVaircraft preliminary designwinglet designaircraft aerodynamicsaircraft dynamic stability |
| spellingShingle | Eleftherios Nikolaou Spyridon Kilimtzidis Vassilis Kostopoulos Winglet Design for Aerodynamic and Performance Optimization of UAVs via Surrogate Modeling Aerospace unmanned air vehicle (UAV) fixed-wing UAV aircraft preliminary design winglet design aircraft aerodynamics aircraft dynamic stability |
| title | Winglet Design for Aerodynamic and Performance Optimization of UAVs via Surrogate Modeling |
| title_full | Winglet Design for Aerodynamic and Performance Optimization of UAVs via Surrogate Modeling |
| title_fullStr | Winglet Design for Aerodynamic and Performance Optimization of UAVs via Surrogate Modeling |
| title_full_unstemmed | Winglet Design for Aerodynamic and Performance Optimization of UAVs via Surrogate Modeling |
| title_short | Winglet Design for Aerodynamic and Performance Optimization of UAVs via Surrogate Modeling |
| title_sort | winglet design for aerodynamic and performance optimization of uavs via surrogate modeling |
| topic | unmanned air vehicle (UAV) fixed-wing UAV aircraft preliminary design winglet design aircraft aerodynamics aircraft dynamic stability |
| url | https://www.mdpi.com/2226-4310/12/1/36 |
| work_keys_str_mv | AT eleftheriosnikolaou wingletdesignforaerodynamicandperformanceoptimizationofuavsviasurrogatemodeling AT spyridonkilimtzidis wingletdesignforaerodynamicandperformanceoptimizationofuavsviasurrogatemodeling AT vassiliskostopoulos wingletdesignforaerodynamicandperformanceoptimizationofuavsviasurrogatemodeling |