G
Guoyan Zhao
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Citation Count:967
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Application of Boundary-Layer Compensation Based on Rough Segment of Scramjet Isolator
基于 scramjet 隔离段粗糙段的边界层补偿应用
AIAA Journal
IF2.8
Effect of shock position on supersonic combustion in a Mach number 8 scramjet combustor
激波位置对Ma 8 scramjet燃烧室超燃流场的影响
The shock-assisted self-ignition behavior and combustion transition mechanisms in a Mach 8 scramjet combustor
Mach 8超燃冲压发动机燃烧室中的冲击辅助自点火行为及燃烧转捩机制
Combustion and Flame
IF6.2
Weak heat release and complex combustion transitions in high-Mach scramjet combustor
高马赫数超燃冲压发动机燃烧室中的弱热释放和复杂的燃烧转捩
On the scale effects of flame stabilization under different combustion modes in an ethylene-fueled scramjet combustor
以乙烯为燃料的超燃冲压发动机燃烧室中不同燃烧模式下火焰稳定的尺度效应
COMBUSTION AND FLAME
IF6.2
Effect of injection scheme on asymmetric phenomenon in rectangular and circular scramjets
喷射方案对矩形和圆形超燃冲压发动机非对称现象的影响

