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Hong-Wei He

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Conference Open access Sep 2026

Cruise aerodynamic performance of a strake-wing tail-sitter UAV

A tail-sitter vertical take-off and landing unmanned aerial vehicle (UAV) for low-altitude interception requires vertical launch capability together with efficient fixed-wing cruise. This study assesses the cruise aerodynamic feasibility of a 30 kg strake-wing concept using three-dimensional steady Reynolds-averaged Na...

Jing-Ming Xiao, Zhi-Yu Wu, Hong-Wei He et al. · 0 citations

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