HVI tests on CFRP laminates at low temperature

被引：36

作者：

Numata, D. ^{[1
]}

Ohtani, K. ^{[2
]}

Anyoji, M. ^{[1
]}

Takayama, K. ^{[3
]}

Togami, K. ^{[4
]}

Sun, M. ^{[5
]}

机构：

[1] Tohoku Univ, Grad Sch Engn, Aoba Ku, Sendai, Miyagi 9808577, Japan

[2] Tohoku Univ, Inst Fluid Sci, Interdisciplinary Shock Wave Res Lab, Aoba Ku, Sendai, Miyagi 9808577, Japan

[3] Tohoku Univ, Biomed Engn Res Org, Aoba Ku, Sendai, Miyagi 9808577, Japan

[4] Mitsubishi Heavy Ind Co Ltd, Nagoya Aerosp Syst Works, Minato Ku, Nagoya, Aichi 4558515, Japan

[5] Tohoku Univ, Interdisciplinary Res Ctr, Sendai, Miyagi 9808578, Japan

来源：

INTERNATIONAL JOURNAL OF IMPACT ENGINEERING | 2008年 / 35卷 / 12期

关键词：

Hypervelocity impact; Low temperature; Space debris bumper shield; Composite material;

D O I：

10.1016/j.ijimpeng.2008.07.055

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

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. (C) 2008 Elsevier Ltd. All rights reserved.

引用

页码：1695 / 1701

页数：7

共 12 条

[1] DESIGN AND PERFORMANCE EQUATIONS FOR ADVANCED METEOROID AND DEBRIS SHIELDS [J].

CHRISTIANSEN, EL .

INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1993, 14 (1-4) :145-156

[2] Impact experiments on low-temperature bumpers [J].

Francesconi, A. ;

Pavarin, D. ;

Giacomuzzo, C. ;

Angrilli, F. .

INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2006, 33 (1-12) :264-272

[3]

*NAT RES COUNC, 1997, PROT SPAC STAT MET O, P10

[4]

National Science and Technology Council Committee on Transportation Research and Development, 1995, INT REP ORB DEBR

[5] A study of hypervelocity impact on cryogenic materials [J].

Ohtani, K. ;

Numata, D. ;

Kikuchi, T. ;

Sun, M. ;

Takayama, K. ;

Togami, K. .

INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2006, 33 (1-12) :555-565

[6] A SIMPLE DYNAMIC-MODEL FOR THE FORMATION OF DEBRIS CLOUDS [J].

PIEKUTOWSKI, AJ .

INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1990, 10 (1-4) :453-471

[7] CHARACTERISTICS OF DEBRIS CLOUDS PRODUCED BY HYPERVELOCITY IMPACT OF ALUMINUM SPHERES WITH THIN ALUMINUM PLATES [J].

PIEKUTOWSKI, AJ .

INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1993, 14 (1-4) :573-586

[8] Fragmentation of a sphere initiated by hypervelocity impact with a thin sheet [J].

Piekutowski, AJ .

INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1995, 17 (4-6) :627-638

[9]

Piekutowski AJ, 1987, Int J Impact Eng, V5, P509

[10] High-speed penetration of a projectile into aluminum alloys at low temperatures [J].

Tanaka, K. ;

Nishida, M. ;

Takada, N. .

INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2006, 33 (1-12) :788-798

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