Equivalent analysis and failure prediction of quasi-isotropic composite sandwich cylinder with lattice core under uniaxial compression

Composite Structures

Volumn 101, Issue , 2013, Pages 180-190

  Sun, Fangfang ^a   Fan, Hualin ^a,b   Zhou, Chuwei ^b   Fang, Daining ^c,d  

^a HOHAI UNIVERSITY   (China)

^b NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

^c TSINGHUA UNIVERSITY   (China)

^d PEKING UNIVERSITY   (China)

Author keywords

Equivalent monocoque shell method; Failure criterion; Mechanical properties; Sandwich cylinder

Indexed keywords

ANALYTICAL INVESTIGATIONS; CARBON FIBER REINFORCED COMPOSITE; COMPOSITE SANDWICHES; EQUIVALENT MONOCOQUE SHELL METHOD; FAILURE CRITERIA; SANDWICH CYLINDERS; SANDWICH CYLINDRICAL SHELLS; UNI-AXIAL COMPRESSION;

BUCKLING; FAILURE MODES; MECHANICAL PROPERTIES;

CYLINDERS (SHAPES);

EID: 84875794801     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2013.02.005     Document Type: Article

References (17)

1. Fan H.L., Fang D.N., Chen L.M., et al. Manufacturing and testing of a CFRC sandwich cylinder with Kagome cores. Compos Sci Technol 2009, 69:2695-2700.
2. Fan H.L., Meng F.H., Yang W. Sandwich panels with Kagome lattice cores reinforced by carbon fibers. Compos Struct 2007, 81:533-539.
3. Vasiliev V.V., Barynin V.A., Rasin A.F. Anisogrid lattice structures survey of development and application. Compos Struct 2001, 54:361-370.
4. Vasiliev V.V., Barynin V.A., Razin A.F. Anisogrid composite lattice structures - development and aerospace applications. Compos Struct 2012, 94:1117-1127.
5. Vasiliev V.V., Razin A.F. Anisogrid composite lattice structures for spacecraft and aircraft applications. Compos Struct 2006, 76:182-189.
6. Agarwal B.L., Sobel L.H. Weight comparisons of optimized stiffened, unstiffened, and sandwich cylindrical shells. J Aircraft 1978, 14:1000-1008.
7. Totaro G. Local buckling modelling of isogrid and anisogrid lattice cylindrical shells with triangular cells. Compos Struct 2012, 94:446-452.
8. Totaro G. Local buckling modelling of isogrid and anisogrid lattice cylindrical shells with hexagonal cells. Compos Struct 2013, 95:403-410.
9. Morozov E.V., Lopatin A.V., Nesterov V.A. Finite-element modelling and buckling analysis of anisogrid composite lattice cylindrical shells. Compos Struct 2011, 93:308-323.
10. Kidane S., Li G.Q., Helms J., et al. Buckling load analysis of grid stiffened composite cylinders. Composites: Part B 2003, 34:1-9.
11. Kim T.D. Fabrication and testing of composite isogrid stiffened cylinder. Compos Struct 1999, 45:1-6.
12. NASA. Isogrid design handbook. NASA CR-124 075, Rev A; 1973.
13. Khalane SA, Babu J, Kumar A, et al. Isogrid design for cylindrical shell. In: Proceedings of the international conference on aerospace science and technology. INCAST 2008-040, Bangalore, India; 26-28 June, 2008.
14. Chen LM. Static and dynamic characteristics of lattice sandwich plates and shells (Dissertation). Beijing: Tsinghua University; 2012.
15. Fan H.L., Yang W. An equivalent continuum method of lattice structures. Acta Mech Solida Sin 2006, 19:103-113.
16. Kollar L., Hegedus I. Analysis and design of space frames by the continuum method 1985, Elsevier Science, Amsterdam.
17. Sun FF. Smearing method of composite sandwich cylinder with lattice cores (Dissertation). Nanjing: Hohai University; 2012.