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Numerical simulation of injection schemes with separate supply of fuel and oxidizer effects on rotating detonation engine
XU Xueyang, ZHUO Changfei, WU Xiaosong, LI Jie, MA Hu
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2016, (4): 1184 -1195 .  DOI: 10.7527/S1000-6893.2015.0195

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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