摘要
给出了复合材料壳体圆筒临界轴压的计算公式。讨论了用壳体内压和轴压实验确定复合材料圆筒弹性常数的工程方法。算例表明 。
The calculation formulae of critical axial compression for the composite case is given. The engineering method for the elastic constants of the composite cylinder defined through the internal pressure test and the axial compression test is discussed. The calculated result is in agreement with the experimental result.
出处
《固体火箭技术》
EI
CAS
CSCD
北大核心
2001年第1期13-15,共3页
Journal of Solid Rocket Technology
