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Panel flutter characteristics on shock wave/boundary layer interaction based on fluid⁃structure coupling
Weijia LIU, Yingkun LI, Xiong CHEN, Chunlei LI
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2023, (6): 127085 -127085 .  DOI: 10.7527/S1000-6893.2022.27085

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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