A comparison of quasi-static indentation and low-velocity impact on composite overwrapped pressure vessels

被引:20
作者
Allen, Trevor [1 ]
Ahmed, Sharif [1 ]
Hepples, Warren [1 ]
Reed, Philippa A. [1 ]
Sinclair, Ian [1 ]
Spearing, Mark [1 ]
机构
[1] Univ Southampton, Fac Engn & Environm, Southampton, Hants, England
基金
英国工程与自然科学研究理事会;
关键词
Hybrid structures; low-velocity impact; quasi-static indentation; computed tomography; DAMAGE; CFRP; THICKNESS; MASS;
D O I
10.1177/0021998318774401
中图分类号
TB33 [复合材料];
学科分类号
摘要
The equivalence of quasi-static indentation and low-velocity impact loading regimes has been assessed for composite overwrapped pressure vessels. Test specimens were assessed in detail in terms of the force-displacement response, and micro-focus computed tomography was used for qualitative and quantitative assessment of the associated damage to the constituent materials/interfaces. The results show that the force-displacement response follows an essentially similar pattern between the two loading regimes (within 10% for all cases). Quantitative assessment of the projected composite damage area and permanent deformation of the aluminium substrate as a function of peak indentor displacement also showed a high degree of equivalence between the loading regimes. It is concluded that quasi-static indentation represents a usable analogue for mechanistic assessment of low-velocity impact damage in the tested composite overwrapped pressure vessels.
引用
收藏
页码:4051 / 4060
页数:10
相关论文
共 23 条
[11]   Energy-based approach to impact damage in CFRP laminates [J].
Delfosse, D ;
Poursartip, A .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 1997, 28 (07) :647-655
[12]   COMPARATIVE ULTRASONIC ANALYSIS OF DAMAGE IN CFRP UNDER STATIC INDENTATION AND LOW-VELOCITY IMPACT [J].
KACZMAREK, H ;
MAISON, S .
COMPOSITES SCIENCE AND TECHNOLOGY, 1994, 51 (01) :11-26
[13]   Effects of stacking thickness on the damage behavior in CFRP composite cylinders subjected to out-of-plane loading [J].
Kobayashi, Satoshi ;
Kawahara, Mari .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2012, 43 (01) :231-237
[14]   A PRELIMINARY PROPOSITION FOR A TEST METHOD TO MEASURE (IMPACT) DAMAGE RESISTANCE [J].
LAGACE, PA ;
WILLIAMSON, JE ;
TSANG, PHW ;
WOLF, E ;
THOMAS, S .
JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 1993, 12 (05) :584-601
[15]   An integrated study on the low-velocity impact response of the GLARE fibre-metal laminate [J].
Moriniere, F. D. ;
Alderliesten, R. C. ;
Sadighi, M. ;
Benedictus, R. .
COMPOSITE STRUCTURES, 2013, 100 :89-103
[16]   Mass criterion for wave controlled impact response of composite plates [J].
Olsson, R .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2000, 31 (08) :879-887
[17]   IMPACTOR MASS AND SPECIMEN GEOMETRY-EFFECTS IN LOW VELOCITY IMPACT OF LAMINATED COMPOSITES [J].
ROBINSON, P ;
DAVIES, GAO .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1992, 12 (02) :189-207
[18]   THE INFLUENCE OF VELOCITY IN LOW-VELOCITY IMPACT TESTING OF COMPOSITES USING THE DROP-WEIGHT IMPACT TOWER [J].
RYDIN, RW ;
BUSHMAN, MB ;
KARBHARI, VM .
JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 1995, 14 (02) :113-127
[19]   Delamination threshold loads for low velocity impact on composite laminates [J].
Schoeppner, GA ;
Abrate, S .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2000, 31 (09) :903-915
[20]   ON LOW-VELOCITY IMPACT TESTING OF COMPOSITE-MATERIALS [J].
SJOBLOM, PO ;
HARTNESS, JT ;
CORDELL, TM .
JOURNAL OF COMPOSITE MATERIALS, 1988, 22 (01) :30-52