您当前的位置：
首页 >
文章列表页 >
基于系统工程模型的飞机总装数字化集成工艺设计方法浅析
更新时间：2025-10-30

    • 基于系统工程模型的飞机总装数字化集成工艺设计方法浅析

    • Aeronautical Manufacturing Technology   Vol. 58, Issue 21, Pages: 73-76(2015)

    • DOI：10.16080/j.issn1671-833x.2015.21.073    

      CLC：

    • Published：2015

    移动端阅览

  • [J]. Aeronautical Manufacturing Technology, 2015, 58(21): 73-76. DOI： 10.16080/j.issn1671-833x.2015.21.073.

  •  
  •  
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

676

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
Large-Distance Straight-Line Datum Construction Based on Laser Collimation
Research Progress on Ceramic Matrix Composites for Aviation Applications
Electromechanical Behavior of Open-Hole Three-Dimensional Angle-Interlock Woven Carbon Fiber Reinforced Polymer Under Tensile Loading
Research on Ultrasonic Vibration-Assisted Milling and Grinding of Ceramic Matrix Composites

Related Author

No data

Related Institution

No data
0