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
Link To Document :
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