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Stationary crossflow induced transition prediction method for supersonic swept-wing based on convolutional neural networks
Jiakun FAN, Junqiang AI, Ningjuan DONG, Jiakuan XU, Lei QIAO, Junqiang BAI
Acta Aeronautica et Astronautica Sinica . 2025, (20): 532012 -532012 .  DOI: 10.7527/S1000-6893.2025.32012

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341