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Starting characteristics of a hypersonic inlet under the influence of near-wall fuel injection
刘思思 徐惊雷 彭元 朱冉 叶涛
Acta Aeronautica et Astronautica Sinica . 0, (): 1 -0 .  DOI: 10.7527/S1000-6893.2026.34276

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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