BENDING FATIGUE DAMAGE MODELS OF STEEL HONEYCOMB SANDWICH PANELS

被引:2
|
作者
Zou Guangping [1 ]
Lu Jie [1 ]
Cao Yang [1 ]
Liu Baojun [1 ]
机构
[1] Harbin Engn Univ, Coll Aerosp & Civil Engn, Harbin 150001, Peoples R China
关键词
honeycomb sandwich; shear modulus degradation; life prediction; cumulative damage; BEHAVIOR; STRENGTH;
D O I
10.3724/SP.J.1037.2011.00253
中图分类号
TF [冶金工业];
学科分类号
0806 ;
摘要
The four-point bending fatigue behaviors of steel honeycomb sandwich panels were investigated in this paper. The fatigue tests results were presented in fatigue life (S-N) diagrams. The results show that with a load ratio of R=0.20, the fatigue properties of specimens are significantly influenced by honeycomb cell orientations. The L-direction appears more suitable for cyclic loading than W-direction, and the fatigue strengths reach 1369 and 859 N, respectively. Based on the equivalent shear modulus degradation theory, the life prediction and damage evolution models were developed. Obviously, the lives of damage initiation for L-direction specimens are 86%-90% of the total number of cycles, while 73% at high load and reduce to 48% at low load for W-direction specimens. When the cores orientations were not concerned, the second order polynomial model and exponential model can be adopted to describe the damage evolution trends at high and low load levels, respectively. While the prediction models exhibit strong material dependent.
引用
收藏
页码:1181 / 1187
页数:7
相关论文
共 20 条
  • [1] Modelling the fatigue behaviour of composites honeycomb materials (aluminium/aramide fibre core) using four-point bending tests
    Abbadi, A.
    Azari, Z.
    Belouettar, S.
    Gilgert, J.
    Freres, P.
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 2010, 32 (11) : 1739 - 1747
  • [2] ASHBY MF, 2006, METAL FOAMS DESIGN G, P115
  • [3] Fatigue analysis of honeycomb-composite sandwich beams
    Belingardi, G.
    Martella, P.
    Peroni, L.
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2007, 38 (04) : 1183 - 1191
  • [4] Experimental investigation of static and fatigue behaviour of composites honeycomb materials using four point bending tests
    Belouettar, S.
    Abbadi, A.
    Azari, Z.
    Belouettar, R.
    Freres, P.
    [J]. COMPOSITE STRUCTURES, 2009, 87 (03) : 265 - 273
  • [5] Modelling the fatigue behaviour of sandwich beams under monotonic, 2-step and block-loading regimes
    Clark, SD
    Shenoi, RA
    Allen, HG
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 1999, 59 (04) : 471 - 486
  • [6] Modelling the flexural behaviour of sandwich composite materials under cyclic fatigue
    El Mahi, A
    Farooq, MK
    Sahraoui, S
    Bezazi, A
    [J]. MATERIALS & DESIGN, 2004, 25 (03) : 199 - 208
  • [7] Analysis of fatigue and damage in glass-fibre-reinforced polypropylene composite materials
    Ferreira, JAM
    Costa, JDM
    Reis, PNB
    Richardson, MOW
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 1999, 59 (10) : 1461 - 1467
  • [8] [符定梅 Fu Dingmei], 2004, [航空精密制造技术, Aviation Precision Manufacturing Technology], V40, P14
  • [9] HWANG W, 1995, J ADV MATER, V26, P3
  • [10] Evaluating bending fatigue strength of aluminum honeycomb sandwich beams using local parameters
    Jen, Yi-Ming
    Chang, Li-Yen
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 2008, 30 (06) : 1103 - 1114