An analytical formulation for the prediction of buckling and postbuckling of composite panels and shells

3rd M.I.T. Conference on Computational Fluid and Solid Mechanics

Volumn , Issue , 2005, Pages 83-87

  Bisagni, Chiara ^a  

^a POLITECNICO DI MILANO   (Italy)

Author keywords

Analytical formulation; Buckling; Composite panels and shells; Finite element analyses; Geometric imperfections; Post buckling field

Indexed keywords

AIRY FUNCTION; ANALYTICAL FORMULATION; ANALYTICAL SOLUTIONS; COMPATIBILITY EQUATION; COMPOSITE LAMINATE; COMPOSITE PANELS; CYLINDRICAL SHELL; FLAT PANEL; GEOMETRIC IMPERFECTION; INITIAL GEOMETRIC IMPERFECTION; KIRCHHOFF HYPOTHESIS; NON-LINEAR FINITE-ELEMENT ANALYSIS; POSTBUCKLING;

COMPUTATIONAL FLUID DYNAMICS; FINITE ELEMENT METHOD; GALERKIN METHODS; LAMINATED COMPOSITES; PLATES (STRUCTURAL COMPONENTS); SHELLS (STRUCTURES);

BUCKLING;

EID: 58349105500     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

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2. Bisagni C, Cordisco P. An experimental investigation into the buckling and post-buckling of CFRP shells under combined axial and torsion loading. Composite Struct 2003;60:391-402.
3. Bisagni C. Numerical analysis and experimental correlation of composite shell buckling and post-buckling. Composites Part B: Eng 2000;31(8):655-667.
4. Levi-Civita T. The absolute differential calculus (Calculus of tensor). New York: Dover Publications, 1977.
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6. Hoskin BC, Baker AA. Composite materials for aircraft structures. New York: AIAA Educational series, 1986.