TECHNICAL PAPERS
Jan 1, 2001

Influence of Residual Strains on Buckling of Thin Filament-Wound Cylinders in Axial Compression

Publication: Journal of Aerospace Engineering
Volume 14, Issue 1

Abstract

This paper describes a method for improving the accuracy of buckling predictions of thin-shell, filament-wound cylinders under axial compression loads using enhanced finite-element models. This is accomplished by incorporating the out-of-plane displacements due to residual strains, in addition to realistic stiffness coupling due to fiber undulations, into finite-element models. The out-of-plane displacements of filament-wound cylinders were scanned mechanically and incorporated into the finite-element models using a computer program. An eigenvalue buckling analysis was performed on these models. Results show that the accuracy of the buckling load prediction of the model with stiffness coupling and out-of-plane displacements due to residual strains is significantly improved compared to the case when only the stiffness coupling is incorporated into the model.

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References

1.
Claus, S. J. ( 1994). “Manufacture-structure performance relationships for filament-wound composite shells.” PhD thesis, Pennsylvania State University, University Park, Pa.
2.
Kapania, R. K. ( 1988). “Analysis of laminated shells. Recent advances in the macro- and micro-mechanics of composite material structures.” Proc., Winter Annu. Meeting of Am. Soc. of Mech. Engrs., ASME, New York, 177–187.
3.
Pai, S. P., and Jensen, D. W. (2001). “Influence of fiber undulations on buckling of thin filament-wound cylinders in axial compression.”J. Aerosp. Engrg., ASCE, 14(1), 12–20.
4.
Singer, J. ( 1982). “Buckling experiments on shells—A review of recent developments.” Solid Mech. Archives, 7, 213–313.
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Tennyson, R. C. ( 1975). “Buckling of laminated composite cylinders: A review.” Compos., 6(1), 17–24.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 14Issue 1January 2001
Pages: 21 - 28

History

Received: Aug 10, 2000
Published online: Jan 1, 2001
Published in print: Jan 2001

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Member, ASCE
Tech. Specialist, Case Corp., Burr Ridge, IL 60521.
Prof. and Dir., Ctr. for Advanced Struct. Compos., Brigham Young Univ., 368 CB, Box 24066, Provo, UT 84602.

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