Ground Servoelasticity Test and Analysis of UAVs With Large Aspect Ratio and Joined-Wing Layout
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DOI: 10.1109/access.2024.3426088
Abstract: Unmanned aerial vehicles (UAVs) with an ultra-large aspect ratio and a joined-wing configuration exhibit characteristics such as minimal mass, remarkable flexibility, and a unified wing structure, thereby presenting a significant challenge in accurately assessing their… read more here.
Keywords: ratio joined; aspect ratio; joined wing; large aspect ... See more keywords
Analysis of Structural Characteristics of the HALE Joined‐Wing Configuration UAV
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DOI: 10.1155/ijae/9931529
Abstract: This study focuses on a high‐altitude long‐endurance (HALE) joined‐wing configuration UAV and completes a preliminary structural design based on aircraft design indices and the fundamental principles of aircraft structure design. Based on the preliminary structural… read more here.
Keywords: configuration; hale; configuration uav; hale joined ... See more keywords
Electric Propulsion Concepts for an Inverted Joined Wing Airplane Demonstrator
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DOI: 10.3390/en10060762
Abstract: One of the airplane design concepts that potentially allows for significantly increased efficiency, but has not yet been investigated thoroughly, is the inverted joined wing configuration, where the upper wing is positioned in front of… read more here.
Keywords: electrical propulsion; propulsion; airplane; demonstrator ... See more keywords