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Impact of pressure variations at inlet and outlet boundaries on aerodynamic performance of multi-stage axial compressor
Cancan LI, Zuoli XIAO, Jiaqi LUO
Acta Aeronautica et Astronautica Sinica . 2024, (19): 630168 -630168 .  DOI: 10.7527/S1000-6893.2024.30168

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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