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Analysis of multifastener composite joints

  • Published:1994-03 Issue:2 Volume:31 Page:278-284
  • ISSN:0022-4650
  • Container-title:Journal of Spacecraft and Rockets
  • language:en
  • Short-container-title:Journal of Spacecraft and Rockets

Author:

Griffin O. H.1,Hyer M. W.1,Cohen D.2,Shuart M. J.3,Yalamanchili S. R.4,Prasad C. B.5

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

2. Hercules Aerospace Company, Magna, Utah 84044

3. NASA Langley Research Center, Hampton, Virginia 23681

4. General Motors Truck Engineering, Warren, Michigan 48091

5. Analytical Services and Materials, Inc., Hampton, Virginia 23666

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Cited by 19 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. References;Handbook of Structural Life Assessment;2017-04-07

2. Numerical method on load sharing problem of thick laminate joints;Journal of Shanghai Jiaotong University (Science);2013-12-04

3. Influence of material and geometrical parameters on stress field of composite plates with insert;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2011-12-07

4. Finite element modeling and optimization of load transfer in multi-fastener joints using structural elements;Composite Structures;2008-01

5. Stress Analysis in Single and Multi Fastened Single-Lap Composite Joints;Key Engineering Materials;2006-03
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