Determination of ply level residual stresses in a laminated carbon fibre-reinforced epoxy composite using constant, linear and quadratic variations of the incremental slitting method

被引:15
|
作者
Gower, M. R. L. [1 ]
Shaw, R. M. [1 ]
Wright, L. [1 ]
Urquhart, J. [1 ]
Hughes, J. [1 ]
Gnaniah, S. [1 ]
Morrell, R. [1 ]
Garstka, T. [2 ]
机构
[1] Natl Phys Lab, Hampton Rd, Teddington TW11 0LW, Middx, England
[2] LMAT Ltd, 128 Stoke Lane, Bristol BS9 3RJ, Avon, England
关键词
Laminates; Residual/internal stress; Computational modelling; Autoclave; LAYER-REMOVAL METHOD; COOL-DOWN; PREDICTION; POLYPROPYLENE; DISTORTION; SURFACE; MATRIX; MODEL;
D O I
10.1016/j.compositesa.2016.08.005
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Measurement of residual stresses in FRP composites is by no means a trivial task and there are no commonly applied or standardised methods currently available. As a result, characterisation of residual stresses is often avoided, resulting in the use of conservative safety margins, which has consequently resulted in structures being overdesigned. In the work described here, the incremental slitting method has been demonstrated to be a technique suitable for measuring residual stress in thin (similar to 0.3 mm) plies of a [0 degrees(2)/90 degrees(2)](4s) carbon fibre-reinforced epoxy laminate. The stresses measured using a constant stress approximation approach provided the best agreement with measurements obtained using the layer removal technique and stresses predicted using a semi-coupled transient-thermal and structural model. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:441 / 450
页数:10
相关论文
共 3 条
  • [1] DETERMINATION OF RESIDUAL STRESSES IN A LAMINATED THERMOSET COMPOSITE USING THE INCREMENTAL SLITTING METHOD
    Gower, Mike
    Shaw, Richard
    Wright, Louise
    Urquhart, Jeannie
    Hughes, Jon
    Gnaniah, Sam
    Morrell, Roger
    Garstka, Tomasz
    20TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS, 2015,
  • [2] Determination of Residual Stresses in GFRP Composite Using Incremental Slitting Method by the Aid of Strain Gauge
    Umarfarooq, M. A.
    Gouda, P. S. Shivakumar
    Nandibewoor, Archana
    Banapurmath, N. R.
    Kumar, G. B. Veeresh
    ADVANCES IN POLYMER COMPOSITES: MECHANICS, CHARACTERIZATION AND APPLICATIONS, 2019, 2057
  • [3] Ply level failure prediction of carbon fibre reinforced laminated composite panels subjected to low velocity drop-weight impact using adaptive meshing techniques
    Farooq, Umar
    Myler, Peter
    ACTA ASTRONAUTICA, 2014, 102 : 169 - 177