Deflagration; Detonations; Energy transfer; Induced environments; Combustion chamber gases; Detonation waves; Acoustic velocity; Subsonic flow; Ducts; Compressors; Stalling; Flames; Fuels; Diluents; Shifting; Hydrogen; Oxygen; Mixtures; Pressure; Heat; Mass; Transitions; Density; Temperature; Mathematical models; Turbojet engines; Afterburners; DDT(Deflagration to Detonation Transition); Chapman Jouquet equations; Induction distance; Frozen speed of sound; Shifting speed of sound; Combustible gas mixtures; Helium; Argon; Carbon dioxide;
机译:脉冲爆震燃烧器流型燃烧室中的循环爆燃-爆轰过渡
机译:NO_2添加对爆燃-爆轰过渡的影响
机译:壁上的热损失和粘滞摩擦对火焰加速和爆燃至爆轰过渡的影响
机译:小型反应炉在逐渐加热下从爆燃到爆燃过渡
机译:流体障碍技术:增强脉冲爆震发动机中爆燃到爆震过渡的一种方法
机译:两相入口质量质量速度流向和加热周长对矩形通道中流沸腾的影响:第1部分–两相流和传热结果
机译:审查影响爆燃的障碍参数(DDT)脉冲爆震发动机应用