Failure prediction on advanced grid stiffened composite cylinder under axial compression

Composite Structures

Volumn 93, Issue 7, 2011, Pages 1939-1946

  Jingxuan, He ^a   Mingfa, Ren ^b   Shiyong, Sun ^b   Qizhong, Huang ^b   Xiannian, Sun ^c  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

^b DALIAN UNIVERSITY OF TECHNOLOGY   (China)

^c DALIAN MARITIME UNIVERSITY   (China)

Author keywords

Advanced grid stiffened (AGS) composite; Failure prediction; Finite element method; Numerical simulation

Indexed keywords

AXIAL COMPRESSION; COMPRESSION TESTING; COMPUTER SIMULATION; CYLINDERS (SHAPES); FORECASTING; NUMERICAL METHODS; NUMERICAL MODELS;

COMPOSITE CYLINDERS; FAILURE PREDICTION; LVDT SENSORS; NUMERICAL RESULTS; STIFFENED COMPOSITE; STRAIN SENSORS;

FINITE ELEMENT METHOD;

EID: 79955483217     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2011.02.003     Document Type: Article

References (19)

1. Vasiliev VV, Razin AF. Anisogrid composite lattice structures for spacecraft and aircraft applications. Compos Struct 2006;76:182-9.
2. Vasiliev VV, Barynin VA, Rasin AF. Anisogrid lattice structures-survey of development and application. Compos Struct 2001;54:361-70.
3. Winterstetter ThA, Schmidt H. Stability of circular cylindrical steel shells under combined loading. Thin-Wall Struct 2002;40:839-909.
4. Key CT, Garnich MR, Hansen AC. Progressive failure predictions for rib stiffened panels based on multi continuum technology. Compos Struct 2004;65:357-66.
5. Higgins PE, Wegner P, Viisoreanu A, Sanford G. Design and testing of the Minotaur advanced grid-stiffened fairing. Compos Struct 2004;66:339-49.
6. Raju IS, Sistla R, Krishnamurthy T. Fracture mechanics analyses for skinstiffener debonding. Eng Fract Mech 1996;54:371-85.
7. Wang JT, Raju IS. Strain energy release rate formulae for skin-stiffener debond modeled with plate elements. Eng Fract Mech 1996;54:211-28.
8. Jeff WH, Scott ML, Rodney ST, Dieter H. The analysis of skin-to-stiffener debonding in composite aerospace structures. Compos Struct 2002;57:425-35.
9. Chen HJ, Tsai SW. Analysis and optimum design of composite grid structures. J Compos Mater 1996;30:503-33.
10. Kolli M, Chandrashekhara K. Finite element analysis of stiffened laminated plates under transverse loading. Compos Sci Technol 1996;56:1335-61.
11. Wu Z, Chen WJ. A new higher-order shear deformation theory based on global-local superposition and refined triangular plate element of composite laminate. J Comput Mech 2005;22:639-45 [in Chinese].
12. ANSYS software, (9.0). ANSYS user's manual, ver. 9.0.
13. Wang XC. Finite element method, 1st ed. Beijing: Tsinghua University Press; 2003.
14. Jones RM. Mechanics of composite materials, 2nd ed. Philadelphia (USA): Taylor & Francis, Inc.; 1998.
15. Chang FK, Lessard LB. Damage tolerance of laminated composite containing an open hole and subjected to compressive loadings: part I - analysis. J Compos Mater 1991;25:2-43.
16. Goyal VK, Jaunky NR, Johnson ER, et al. Intralaminar and interlaminar progressive failure analyses of composite panels with circular cutouts. Compos Struct 2004;64:91-105.
17. Yang J, Fu Y, Wang X. Variational analysis of delamination growth for composite laminated cylindrical shells under circumferential concentrated load. Compos Sci Technol 2007;67:541-50.
18. Camanho PP, Matthews FL. A progressive damage model for mechanically fastened joints in composite laminates. J Compos Mater 1999;33:2248-80.
19. Huybrechts SM, Tsai SW. Analysis and behavior of grid structure. Compos Sci Technol 1996;56:1001-15.