Buckling of Composite Cylindrical Characterization Specimens
- 1 April 1975
- journal article
- research article
- Published by SAGE Publications in Journal of Composite Materials
- Vol. 9 (2) , 138-148
- https://doi.org/10.1177/002199837500900204
Abstract
Using dimensions which are typical of current laboratory tubular specimens, critical buckling loads are determined'for unidirectional and Jaminated cylinders subjected to torsion and to axial compression. Buckling loads are obtained by using classical Fourier analysis in conjunction with Flugge's shell equations modified for anisotropic laminated materials. Comparison of buckling loads to composite strength, as estimated from maximum strain criterion, suggests that buckling is a potential problem in the use of tubular specimens. A relatively easy method for estimating buckling loads is also presented.This publication has 11 references indexed in Scilit:
- Effect of end attachment on the strength of fiber-reinforced composite cylindersExperimental Mechanics, 1973
- Pure Bending of Helical Wound Composite CylindersPublished by ASTM International ,1973
- Analysis of anisotropic rectangular plates.AIAA Journal, 1972
- Free Vibration of Anisotropic Rectangular PlatesThe Journal of the Acoustical Society of America, 1972
- Fourier Analysis of Clamped Anisotropic PlatesJournal of Applied Mechanics, 1971
- On the Use of Shell Theory for Determining Stresses in Composite CylindersJournal of Composite Materials, 1971
- Stress Gradients in Laminated Composite CylindersJournal of Composite Materials, 1971
- Geometric Design of Composite Cylindrical Characterization SpecimensJournal of Composite Materials, 1970
- STABILITY OF HETEROGENEOUS AEOLOTROPIC CYLINDRICAL SHELLS UNDER COMBINED LOADINGAIAA Journal, 1963
- Double Fourier series and boundary value problemsMathematical Proceedings of the Cambridge Philosophical Society, 1944