HVI tests on CFRP laminates at low temperature

D. Numata, K. Ohtani, Masayuki Anyoji, K. Takayama, K. Togami, M. Sun

Research output: Contribution to journalArticle

21 Citations (Scopus)

Abstract

The paper reports a result of low temperature hypervelocity impact (HVI) tests of aluminum sphere against a 16-ply quasi-isotropic Carbon Fiber Reinforced Plastic (CFRP) laminate plate at speed ranging from 1.4 to 5.4 km/s in air at 10 Pa. The result was compared with room temperature impacts. At low speed impact on CFRP plates, fracture patterns of specimens varied depending on their temperatures, whereas at high-speed impact, any significant differences in the fracture patterns around penetration holes and independent of the temperatures.

Original languageEnglish
Pages (from-to)1695-1701
Number of pages7
JournalInternational Journal of Impact Engineering
Volume35
Issue number12
DOIs
Publication statusPublished - Dec 1 2008
Externally publishedYes

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Plastic laminates
Carbon fiber reinforced plastics
Temperature
Aluminum
Air

All Science Journal Classification (ASJC) codes

  • Safety, Risk, Reliability and Quality
  • Ocean Engineering
  • Automotive Engineering
  • Aerospace Engineering
  • Civil and Structural Engineering
  • Mechanics of Materials
  • Mechanical Engineering

Cite this

HVI tests on CFRP laminates at low temperature. / Numata, D.; Ohtani, K.; Anyoji, Masayuki; Takayama, K.; Togami, K.; Sun, M.

In: International Journal of Impact Engineering, Vol. 35, No. 12, 01.12.2008, p. 1695-1701.

Research output: Contribution to journalArticle

Numata, D, Ohtani, K, Anyoji, M, Takayama, K, Togami, K & Sun, M 2008, 'HVI tests on CFRP laminates at low temperature', International Journal of Impact Engineering, vol. 35, no. 12, pp. 1695-1701. https://doi.org/10.1016/j.ijimpeng.2008.07.055
Numata, D. ; Ohtani, K. ; Anyoji, Masayuki ; Takayama, K. ; Togami, K. ; Sun, M. / HVI tests on CFRP laminates at low temperature. In: International Journal of Impact Engineering. 2008 ; Vol. 35, No. 12. pp. 1695-1701.
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