Numerical study on drag reduction and lift enhancement of a swept wing at high Mach number based on pulsed plasma actuations

YAN Yilun; GUO Dechun

doi:10.13700/j.bh.1001-5965.2025.0462

Article Contents

Journal of Beijing University of Aeronautics and Astronautics > 2025 > Accepted Manuscript

YAN Yilun, GUO Dechun. Numerical study on drag reduction and lift enhancement of a swept wing at high Mach number based on pulsed plasma actuations[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2025.0462(in Chinese)

Citation:

YAN Yilun, GUO Dechun. Numerical study on drag reduction and lift enhancement of a swept wing at high Mach number based on pulsed plasma actuations[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2025.0462(in Chinese)