您当前的位置:
首页 >
文章列表页 >
常幅法向压力下飞机舱门锁机构磨损特性*
更新时间:2026-04-17
    • 常幅法向压力下飞机舱门锁机构磨损特性*

    • Aeronautical Manufacturing Technology   Vol. 59, Issue 9, Pages: 84-87(2016)
    • DOI:10.16080/j.issn1671-833x.2016.09.084    

      CLC:
    • Published:2016

    移动端阅览

  • 郭兰中, 林化清, 许文文. 常幅法向压力下飞机舱门锁机构磨损特性*[J]. Aeronautical Manufacturing Technology, 2016, 59(9): 84-87. DOI: 10.16080/j.issn1671-833x.2016.09.084.

  •  
  •  
icon
试读结束,您可以激活您的VIP账号继续阅读。
去激活 >
icon
试读结束,您可以通过登录账户,到个人中心,购买VIP会员阅读全文。
已是VIP会员?
去登录 >

0

Views

408

下载量

0

CSCD

Alert me when the article has been cited
提交
Tools
Download
Export Citation
Share
Add to favorites
Add to my album

Related Articles

Design and Experimental Verification of Stitching Forming System for Rigid Sandwich Composite Preforms
Research Progress on Matrix Composition Regulation of SiC/SiC Composites
Research Progress on Ceramic Matrix Composites for Aviation Applications
Assessment of Technological Advancement Based on Fuzzy Comprehensive Evaluation
Electromechanical Behavior of Open-Hole Three-Dimensional Angle-Interlock Woven Carbon Fiber Reinforced Polymer Under Tensile Loading

Related Author

No data

Related Institution

No data
0