一种增强航天飞行器用圆柱壳结构气动弹性稳定性的方法
Release time:2024-11
Hits:
- Patent description:
- 一种增强航天飞行器用圆柱壳结构气动弹性稳定性的方法，发明专利，申请号：CN202010071447.3
- Service Invention or Not:
- no
- Pre One:基于超高速下飞行器的梁结构提高气动弹性稳定性设计方法
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