Experimental and numerical study on buckling of axially compressed composite cylinders
Thin shells are lightweight, efficient structures that can support very high buckling loads. However, unlike columns and plates, shells usually have a very unstable post-buckling behaviour that strongly influences their buckling characteristics. Axially compressed cylinder may be one of the last cla...
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Published in | Rigas Tehniskas Universitates Zinatniskie Raksti Vol. 10; no. 10; pp. 33 - 49 |
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Main Authors | , , |
Format | Journal Article |
Language | English |
Published |
Riga
Versita
01.01.2009
Riga Technical University |
Subjects | |
Online Access | Get full text |
ISSN | 1407-7329 2255-8551 |
DOI | 10.2478/v10137-009-0004-2 |
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Abstract | Thin shells are lightweight, efficient structures that can support very high buckling loads. However, unlike columns and plates, shells usually have a very unstable post-buckling behaviour that strongly influences their buckling characteristics. Axially compressed cylinder may be one of the last classical problems in structural mechanics for which it remains difficult to obtain close agreement between careful experiments and the best predictions from numerical modelling, and therefore much more research is needed on this subject. Within this investigation, 18 glass fibre composite shells with wall thickness of 1.1 mm, 0.3 m and 0.5 m diameters and various lengths have been produced along with flat specimens for determination of elastic properties of the material. The cylinders were repeatedly loaded until post-buckling and load-shortening curves and pictures of buckling mode shapes have been registered. Finite element models of the specimens have been developed in ABAQUS finite element package and non-linear explicit dynamic analyses have been performed for comparison with experimental and analytical results. Gradually improving the finite element model and adding artificial initial imperfections resulted in good agreement between the experimental and numerically obtained critical loads. The buckling modes observed during the experiments are in good agreement with the results of finite element simulations as well. |
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AbstractList | Thin shells are lightweight, efficient structures that can support very high buckling loads. However, unlike columns and plates, shells usually have a very unstable post-buckling behaviour that strongly influences their buckling characteristics. Axially compressed cylinder may be one of the last classical problems in structural mechanics for which it remains difficult to obtain close agreement between careful experiments and the best predictions from numerical modelling, and therefore much more research is needed on this subject. Within this investigation, 18 glass fibre composite shells with wall thickness of 1.1 mm, 0.3 m and 0.5 m diameters and various lengths have been produced along with flat specimens for determination of elastic properties of the material. The cylinders were repeatedly loaded until post-buckling and load-shortening curves and pictures of buckling mode shapes have been registered. Finite element models of the specimens have been developed in ABAQUS finite element package and non-linear explicit dynamic analyses have been performed for comparison with experimental and analytical results. Gradually improving the finite element model and adding artificial initial imperfections resulted in good agreement between the experimental and numerically obtained critical loads. The buckling modes observed during the experiments are in good agreement with the results of finite element simulations as well. |
Author | Eglītis, Edgars Ozoliņš, Oļgerts Kalniņš, Kaspars |
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Cites_doi | 10.1098/rsta.1914.0005 10.4324/9780203301609 10.2514/8.3911 10.1115/1.3564613 10.2514/3.61860 10.1090/qam/99838 10.1016/S0263-8223(01)00053-8 10.1016/S0263-8223(03)00024-2 |
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References_xml | – volume: 5 start-page: 26 year: 1967 ident: 4 article-title: Thin Shells in Aerospace Structures publication-title: Aeronautics and Astronautics – ident: 18 – volume: 213 start-page: 187 year: 1914 ident: 7 publication-title: Philosophical Transactions of the Royal Society doi: 10.1098/rsta.1914.0005 – volume-title: Buckling Experiments: Experimental Methods in Buckling of Thin-Walled Structures year: 2004 ident: 1 – volume-title: Buckling of Thin Metal Shells year: 2004 ident: 2 doi: 10.4324/9780203301609 – start-page: 67 year: 1906 ident: 3 article-title: The Economic Design Of Columns publication-title: Transactions of Institution of Civil Engineers of Ireland (Dublin) – volume: 24 start-page: 587 year: 1957 ident: 24 article-title: The stability of thin-walled unstiffened circular cylinders under axial compression including the effects of internal pressure publication-title: Journal of Aeronautical Science doi: 10.2514/8.3911 – volume: 36 start-page: 233 year: 1969 ident: 10 article-title: The Buckling of a Column with Random Initial Deflections publication-title: Journal of Applied Mechanics doi: 10.1115/1.3564613 – start-page: 498 year: 1991 ident: 14 article-title: Buckling Tests with Axially Compressed Unstiffened Cylindrical Shells Made from CFRP – year: 1991 ident: 15 article-title: Buckling Behavior of Composite Shells under Combined Loading – volume: 10 start-page: 143 year: 1973 ident: 12 article-title: Buckling of Laminated Anisotropic Imperfect Circular Cylinders under Axial Compression publication-title: Journal of Spacecraft doi: 10.2514/3.61860 – volume: 26 start-page: 537 year: 1969 ident: 11 article-title: Buckling under Axial Compression of Long Cylindrical Shells with Random Axisymmetric Imperfections publication-title: Quarterly of Applied Mathematics doi: 10.1090/qam/99838 – year: 1962 ident: 9 article-title: Statistical Methods in the Nonlinear Theory of Shells – volume: 58 start-page: 378 year: 1910 ident: 6 article-title: Einige Stabilitätsprobleme der Elasticitätstheorie publication-title: Zeitschrift für Matematic und Physik – start-page: 101 year: 2007 ident: 8 article-title: Numerical Study of Geometrical Imperfection Response on Composite Cylinders under Axial Loading – start-page: 411 year: 1996 ident: 13 article-title: Buckling Research for Imperfection Tolerant Fiber Composite Structures – start-page: 32 year: 2007 ident: 22 article-title: Benchmarking of FE post-buckling analysis of stiffened composite panels with experimental validation – volume: 52 start-page: 1766 year: 1908 ident: 5 article-title: Buckling of cylindrical shell shell under axial compression publication-title: Zeitschrift des Vereines Deutcher Ingenieure – volume: 53 start-page: 427 year: 2001 ident: 16 article-title: Buckling Loads of CFRP Composite Cylinders under Combined Axial and Torsion Loading - Experiments and Computations publication-title: Composite Structures doi: 10.1016/S0263-8223(01)00053-8 – start-page: 76 year: 2008 ident: 19 article-title: An experimental and numerical study on the dynamic buckling of cylindrical composite shells – ident: 21 – volume: 60 start-page: 391 year: 2003 ident: 17 article-title: An Experimental Investigation into the Buckling and Post-buckling of CFRP Shells under Combined Axial and Torsion Loading publication-title: Composite Structures doi: 10.1016/S0263-8223(03)00024-2 – ident: 20 – ident: 23 |
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Snippet | Thin shells are lightweight, efficient structures that can support very high buckling loads. However, unlike columns and plates, shells usually have a very... |
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SubjectTerms | axially compressed cylinders Buckling buckling experiments composite shells Computer simulation Cylinders Finite element method imperfecitons Mathematical analysis Mathematical models Shells Thin walled shells |
Title | Experimental and numerical study on buckling of axially compressed composite cylinders |
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