Buckling loads of CFRP composite cylinders under combined axial and torsion loading - experiments and computations

Citation
Hr. Meyer-piening et al., Buckling loads of CFRP composite cylinders under combined axial and torsion loading - experiments and computations, COMP STRUCT, 53(4), 2001, pp. 427-435
Citations number
3
Categorie Soggetti
Material Science & Engineering
Journal title
COMPOSITE STRUCTURES
ISSN journal
02638223 → ACNP
Volume
53
Issue
4
Year of publication
2001
Pages
427 - 435
Database
ISI
SICI code
0263-8223(200109)53:4<427:BLOCCC>2.0.ZU;2-F
Abstract
During the years 1994 through 1999, a European research project under the t itle "Design and Validation of Imperfection-Tolerant Laminated Shells" (DEV ILS) was carried out. In this project, 11 European partners were involved. A goal of the project was an analytical and experimental study of the buckl ing behavior of thin-walled carbon fibre reinforced polymer (CFRP) laminate d shells under combined axial and torsion loading. An additional aim was to compose a guideline for the dimensioning of such shells. This paper deals with the experimental and the analytical work conducted by DLR (Institute o f Structural Mechanics, Braunschweig), ETH Zurich (former Institute of Ligh tweight Structures and Ropeways) and EMPA Dubendorf (Department of Polymers /Composites) in that project. The study was aimed at the determination of b uckling loads of circular cylindrical shells of different laminate lay-ups. Nine shells were tested at DLR in Braunschweig for axial compression and a t EMPA in Dubendorf under axial load and under combined axial compression a nd superimposed torsion. To determine the geometrical quality, the internal and the external surfaces of the specimens were mapped. ETH used photogram metry and laser scanning prior to loading, while EMPA applied coordinate me asurements for the unloaded shells and Moire projection to monitor the late ral deflection of the cylindrical wall during loading and after buckling. A t DLR, strain measurements were performed to assess regularity of the load distribution throughout the loading. The investigation showed that buckling loads of cylinders which are imperfection-sensitive under axial loading ma y not be so sensitive to combined loads. Furthermore, it was found that the stiffness eccentricity of the laminate played a significant role on the ma gnitude of the axial buckling load, while for combined loads this effect wa s somewhat reduced. This paper contains the results of those tests and also the comparison with results of analytical investigations and FE modeling; the obtained data can be used as benchmark reference. (C) 2001 Elsevier Sci ence Ltd. All rights reserved.