Testing of Stiffened Composite Cylindrical Shells in the Postbuckling Range Until Failure

Abstract

The results of an experimental investigation of two stringer-stiffened shells and of two ring- and stringer-stiffened cylindrical shells made of carbon fabric reinforced plastic are presented. The pecimens are tested until collapse by means of custom-made biaxial testing equipment that allows axial and torsion loading, applied separately and in combination, using a position control mode. This apparatus includes a laser scanning system for the measurement in situ of the geometric mperfections, as well as of the progressive change in deformations. The experimental data acquired during the first nondestructive buckling tests and during the destructive failure tests clearly demonstrate the strength capacity of these structures to work in the postbuckling field, allowing for the further weight savings likely to be requested in the near future for the construction of aerospace structures. Indeed, the results show that the shells are able to sustain load in the postbuckling field without any damage, whereas the collapse, both under axial compression and under torsion, due to the failure of the stringers is sudden and destructive. The measured data can be used for the development and validation of analytical and numerical high-fidelity methods and, together to these validated analysis tools, to provide design criteria that are less conservative than those presented

Towards imperfection insensitive buckling response of shell structures-shells with plate-like post-buckled responses

“…

Figure 1.Composite shells designs for reduced imperfection sensitivity. (a) Axially stiffened (7) , (b) Variable-stiffness (curvilinear fibres) (11) , (c) Hybrid glass-carbon-reinforced epoxy (12) , (d) ‘Wavy’ shell design. (13)

…”

Design and analysis of stiffened composite panels including post-buckling and collapse

“…Collapse is specified by that point of the load-displacement curve where a sharp decrease occurs thus limiting the load-carrying capacity. The POSICOSS team developed fast and reliable procedures for post-buckling analysis of fibre composite stiffened panels, created experimental data bases and derived design guidelines [1,2,[5][6][7][8][9][10][11][12][13][14][15][16][17]. Alternative fast methods were developed also in parallel to the POSICOSS project [17][18][19][20].…”

Buckling Analysis of Stiffened Panels Under Fuselage Bending

“…The FEM transforms the elliptic PDE into algebraic equations set, that are simple to solve. The initial value problems which has hyperbolic or parabolic differential equation and initial conditions not completely solved by the FEM [7,8]. The hyperbolic or parabolic differential equations contain one independent variables as time.…”