您当前的位置:
首页 >
文章列表页 >
ANALYSIS OF RIVETING CARRYING CAPACITY FOR COMPOSITE TAIL SHAFT OF HELICOPTER TRANSMISSION SYSTEM
更新时间:2022-09-22
    • ANALYSIS OF RIVETING CARRYING CAPACITY FOR COMPOSITE TAIL SHAFT OF HELICOPTER TRANSMISSION SYSTEM

    • Journal of Mechanical Strength   Vol. 41, Issue 2, Pages: 488-492(2019)
    • 作者机构:

      1. 中国航发湖南动力机械研究所

    • DOI:10.16579/j.issn.1001.9669.2019.02.039    

      CLC:

    扫 描 看 全 文

  • YANG XianKun, XIE JunLing, WAN ZhenHua, et al. ANALYSIS OF RIVETING CARRYING CAPACITY FOR COMPOSITE TAIL SHAFT OF HELICOPTER TRANSMISSION SYSTEM. [J]. 41(2):488-492(2019) DOI: 10.16579/j.issn.1001.9669.2019.02.039.

  •  

0

Views

208

下载量

2

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

STUDY ON BEND-TWIST COUPLING CHARACTERISTICS OF WEB OFFSET FOR LARGE WIND TURBINE BLADES (MT)
THREE POINT BENDING PERFORMANCE OF COMPOSITE HONEYCOMB SANDWICH STRUCTURE (MT)
STUDY ON THE STRUCTURAL CHARACTERISTICS OF LARGE WIND TURBINE COMPOSITE BLADE BASED ON BEND-TWIST COUPLING
STUDY ON LOW VELOCITY IMPACT CHARACTERISTICS OF HYBRID COMPOSITE HONEYCOMB SANDWICH STRUCTURE
STUDY ON LATERAL AND LONGITUDINAL STIFFNESS CHARACTERISTICS OF LONG ROUND BELLOW-TYPE AIRBAG ISOLATOR

Related Author

No data

Related Institution

School of Energy and Power Engineering, University of Shanghai for Science and Technology
Shanghai Key Laboratory of Multiphase Flow and Heat Transfer in Power Engineering
Institute of Applied Mechanics, College of Mechanical and Vehicle Engineering, Taiyuan University of Technology
State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace,Xi′an Jiaotong University
Huayang New Material Technology Group Co., Ltd.
0