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Full flow path performance design method for wide range scramjet based on equivalent thermodynamic process
Bing WAN, Jun CHEN, Hanchen BAI
Acta Aeronautica et Astronautica Sinica . 2024, (4): 128757 -128757 .  DOI: 10.7527/S1000-6893.2023.28757

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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