摘要
本文提出了侧向柔度法。该方法把壳体的侧向柔度率作为控制参数,研究该参数随轴压的变化特性,结合低载荷下的实测数据,运用最小二乘法原理进行拟合,可预示失稳载荷。计算实例表明,这种方法是可行的。
A new nondestructive test method, which is called as lateral flexibility method, is provided in this paper. The method based on extrapolation using “lateral flexibility rate” as control variation. critical loads of cylindrical shells can be predicted by analysising date measured under lower load, and applying principle of the method of least square.
出处
《宇航学报》
EI
CAS
CSCD
北大核心
1989年第2期53-60,共8页
Journal of Astronautics
关键词
壳体
非破坏预示
载荷
航天器
Nondestructive test, Stability analysis, Cylindrical structure,Perturbation method.