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Materials Research Innovations Volume 19, 2015 - Issue sup5: Global Conference on Materials Science and Engineering (CMSE 2014)
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Research Papers

Experimental study on composite stiffened panel with low velocity impact damage under compressive load

T. AnAeronautics and Astronautics Engineering CollegeAir Force Engineering University, Xi'an, Shanxi710038, China
,
Y. HeAeronautics and Astronautics Engineering CollegeAir Force Engineering University, Xi'an, Shanxi710038, ChinaCorrespondence[email protected]
,
Q. ShaoAeronautics and Astronautics Engineering CollegeAir Force Engineering University, Xi'an, Shanxi710038, China
&
J. WangAeronautics and Astronautics Engineering CollegeAir Force Engineering University, Xi'an, Shanxi710038, China
Pages S5-861-S5-864 | Received 20 Oct 2014, Accepted 18 Dec 2014, Published online: 30 May 2015

References

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  • X. Zhang: ‘Low velocity impact analysis based on pit depth’, PhD thesis, Xi'an Northwestern Polytechnical University, China, 2010, 2–3.
  • Q. Shao and Y. He: ‘Experiment on composite stiffened panel with through-thickness damage under compress load’, J. Mech. Strength, 2012, 34, 662–665.
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  • W. Lu, Y. C. Ma, W. Liang and Z. Lu: ‘Analysis system of stability and strength for airframe composite stiffened plate/shell’, Acta Aeronaut. Astronaut. Sin., 2009, 30, 896–900.

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