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Aerodynamic design and wind tunnel test on the inward-turning inlet of high-speed rocket-augmented ramjet engine
杨一言 傅岸祥 王昱辉 田照阳 石磊
Acta Aeronautica et Astronautica Sinica . 0, (): 1 -0 .  DOI: 10.7527/S1000-6893.2025.32202

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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