TECHNICAL PAPERS
Mar 1, 2000

Behavior and Design of Concentrically Loaded Pultruded Angle Struts

Publication: Journal of Structural Engineering
Volume 126, Issue 3

Abstract

This paper presents the results of a study pertaining to the short-term behavior of concentrically loaded single angle members made of pultruded fiber-reinforced polymeric materials. Seven E-glass/polyester and 18 E-glass/vinylester angle specimens having slenderness ratios ranging from 30 to 105 and leg width-to-thickness ratios of 8, 10.7, 12, 16, and 24 were tested. Tests have shown that under compression loading, pultruded angles reinforced with E-glass roving and nonwoven E-glass strand mats buckle in either flexural or flexural-torsional modes. These experimentally observed buckling modes were also predicted analytically, based on derived mathematical models that describe the buckling behavior of a specially orthotropic, centrally loaded, equal-leg angle section. Compression and in-plane shear coupon tests were conducted to characterize the material. The results were analyzed statistically to obtain the 95% lower confidence limit on the 5th percentile strength and modulus values, which in turn were used in the analytical buckling formulae to correlate the experimental to the analytical buckling loads. Finally, load and resistance factor design equations with a target reliability index of 3 for buckling and 4 for material compressive strength limit states are proposed.

Get full access to this article

View all available purchase options and get full access to this article.

References

1.
Adluri, M. R., and Madugula, M. (1996). “Torsional-flexural buckling strength of steel angles.” Can. J. Civ. Engrg., 23, 260–271.
2.
Bain, L. J., and Englehardt, M. (1991). Statistical analysis of reliability and life-testing models—Theory and methods, 2nd Ed., Marcel Dekker, New York.
3.
Bauld, N. R., and Tzeng, L. (1984). “A Vlasov theory for fiber-reinforced beams with thin-walled open cross sections.” Int. J. Solids and Struct., 20(3), 277–297.
4.
Ellingwood, B., MacGregor, J. G., Galambos, T. V., and Cornell, C. A. (1982). “Probability-based load criteria: Load factors and load combinations.”J. Struct. Div., ASCE, 108(5), 978–977.
5.
Galambos, T. V. (1998). Guide to stability design criteria for metal structures. 5th Ed., Wiley, New York.
6.
Haiijer, G. ( 1959). “Plate buckling in the strain-hardening range.” Paper No. 2968, Trans., ASCE, 124, 117–148.
7.
Hewson, P. J. (1978). “Buckling of pultruded glass fibre-reinforced channel sections.” Composites, January, 56–60.
8.
Holston, A. (1970). “Buckling of orthotropic plates with one free edge.” AIAA J., 8(7), 1352–1354.
9.
Lawless, J. F. (1982). Statistical models and methods for lifetime data. Wiley, New York.
10.
Mann, N. R., Scheuer, E. M., and Fertig, K. W. (1973). “A new goodness of fit for the two-parameter Weibull or extreme value distribution.” Commun. Stat., 2, 383–400.
11.
Marsh, C. (1997). “Design of single and multiple angle columns and beams.”J. Struct. Engrg., ASCE, 123(7), 847–856.
12.
“Standard specification for dimensional tolerance of thermosetting glass-reinforced plastic pultruded shapes.” (1994). D3917-94, ASTM, West Conshohoken, Pa.
13.
“Standard test method for compressive properties of polymer matrix composite materials with unsupported gauge section by shear loading.” (1995). D3410/D3410M-95, ASTM, West Conshohoken, Pa
14.
“Standard test method for shear properties of composite materials by the V-notched beam method.” (1993). D5379/5379M-93, ASTM, West Conshohoken, Pa.
15.
Trayer, G. W., and March, H. W. (1931). “Elastic instability of members having sections common in aircraft construction.” NACA Rep. No. 382, Washington, D.C.
16.
Ye, B. S., Svenson, A. L., and Bank, L. C. (1995). “Mass and volume fraction properties of pultruded glass fibre-reinforced composites.” Composites, 26, 725–731.
17.
Zureick, A. (1998). “FRP pultruded structural shapes.” Progress in Struct. Engrg. and Mat., 1(2), 143–149.
18.
Zureick, A., and Scott, D. (1997). “Short-term behavior of fiber-reinforced polymeric slender members under axial compression.”J. Compos. for Constr., ASCE, November, 140–149.

Information & Authors

Information

Published In

Go to Journal of Structural Engineering
Journal of Structural Engineering
Volume 126Issue 3March 2000
Pages: 406 - 416

History

Received: Mar 2, 1999
Published online: Mar 1, 2000
Published in print: Mar 2000

Permissions

Request permissions for this article.

Authors

Affiliations

Prof., Struct. Engrg., Mech., and Mat., Georgia Inst. of Technol., Atlanta, GA 30332.
Asst. Prof., Dept. of Civ. Engrg., Univ. of New Hampshire, Durham, NH 03824.

Metrics & Citations

Metrics

Citations

Download citation

If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.

Cited by

View Options

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Media

Figures

Other

Tables

Share

Share

Copy the content Link

Share with email

Email a colleague

Share