The shallow cylindrical shell is a typical type of structure of aircraft.
圆柱形扁壳是飞行器的常见结构形式。
The cylindrical shell, reinforced with non-uniform circular ring-frames, is a new structure of submersible pressure hulls.
本文应用能量法推导了一种新型的潜水器耐压壳结构——非匀加肋圆柱壳总失稳压力的计算公式。
A very good base is made for designing the structure of longitudinal-transverse stiffened cylindrical shell.
为开展纵横加肋圆柱壳的结构设计打下了良好的基础。
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