Title of article
HVI tests on CFRP laminates at low temperature
Author/Authors
D. Numata، نويسنده , , K. Ohtani، نويسنده , , M. Anyoji، نويسنده , , K. Takayama، نويسنده , , K. Togami، نويسنده , , M. Sun، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2008
Pages
7
From page
1695
To page
1701
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.
Keywords
hypervelocity impact , low temperature , Space debris bumper shield , composite material
Journal title
International Journal of Impact Engineering
Serial Year
2008
Journal title
International Journal of Impact Engineering
Record number
1251558
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