Release Time:2019-12-10 Hits:
First Author: 王博
Disigner of the Invention: 蒋亮亮,黄诚,任明法,杜凯繁,Bi Xiangjun,Peng Hao
Authorization Number: 2016107123995
Prev One:一种优化的轻质钛合金快速成型运载火箭捆绑支座的制备方法
Next One:基于孔隙尺寸识别的含孔隙复合材料力学性能测量系统及方法