您当前的位置：
首页 >
文章列表页 >
型号合格取证过程适航知识要素分析与系统建模
更新时间：2025-10-30

    • 型号合格取证过程适航知识要素分析与系统建模

    • Aeronautical Manufacturing Technology   Vol. 58, Issue 3, Pages: 97-101(2015)

    • DOI：10.16080/j.issn1671-833x.2015.03.097    

      CLC：

    • Published：2015

    移动端阅览

  • [J]. Aeronautical Manufacturing Technology, 2015, 58(3): 97-101. DOI： 10.16080/j.issn1671-833x.2015.03.097.

  •  
  •  
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

493

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

Research Progress on In-Plane Shear Mechanical Behavior of Silicon Carbide Ceramic Matrix Composites
Large-Distance Straight-Line Datum Construction Based on Laser Collimation
Research on Ultrasonic Vibration-Assisted Milling and Grinding of Ceramic Matrix Composites
Design and Experimental Verification of Stitching Forming System for Rigid Sandwich Composite Preforms
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