Numerical simulation of directional stability augmentation of a low-aspect-ratio flying wing through symmetric deflection of all-moving wingtips

JIANG Yun; LI Daochun; KAN Zi; SUN Runze; XIANG Jinwu

doi:10.13700/j.bh.1001-5965.2026.0495

Article Contents

Journal of Beijing University of Aeronautics and Astronautics > 2026 > Accepted Manuscript

JIANG Yun, LI Daochun, KAN Zi, et al. Numerical simulation of directional stability augmentation of a low-aspect-ratio flying wing through symmetric deflection of all-moving wingtips[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2026.0495(in Chinese)

Citation:

JIANG Yun, LI Daochun, KAN Zi, et al. Numerical simulation of directional stability augmentation of a low-aspect-ratio flying wing through symmetric deflection of all-moving wingtips[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2026.0495(in Chinese)

Citation:

JIANG Yun, LI Daochun, KAN Zi, et al. Numerical simulation of directional stability augmentation of a low-aspect-ratio flying wing through symmetric deflection of all-moving wingtips[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2026.0495(in Chinese)

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