热蒸汽被喷口边缘冷却、压缩并最终形成了喷口边缘的冰柱。
The steam is cooled by the cold engine nozzle, condensing and eventually freezing at the nozzle exit to form icicles.
在任意曲线坐标系下对带有横向波纹隔热屏、外冷却通道和尾喷口的涡喷加力燃烧室的三维热态流场进行数值模拟。
The flow field calculation and buckling analysis were conducted for the afterburner with a heat shield, flame stabilizer and jet nozzle.
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