Title page for ETD etd-12052003-154555

Type of Document Dissertation
Author Hayes, Michael David
Author's Email Address mdhayes@vt.edu
URN etd-12052003-154555
Title Structural Analysis of a Pultruded Composite Beam: Shear Stiffness Determination and Strength and Fatigue Life Predictions
Degree PhD
Department Engineering Science and Mechanics
Advisory Committee
Advisor Name Title
Lesko, John J. Committee Chair
Case, Scott W. Committee Member
Cousins, Thomas E. Committee Member
Hajj, Muhammad R. Committee Member
Hyer, Michael W. Committee Member
  • finite element analysis
  • beam theory
  • fatigue life
  • remaining strength
  • strength
  • durability
  • FRP beam
  • compression
  • delamination
  • Timoshenko shear stiffness
Date of Defense 2003-11-18
Availability unrestricted
This dissertation is focused on understanding the performance of a particular fiber-reinforced polymeric composite structural beam, a 91.4 cm (36 inch) deep pultruded double-web beam (DWB) designed for bridge construction. Part 1 focuses on calculating the Timoshenko shear stiffness of the DWB and understanding what factors may introduce error in the experimental measurement of the quantity for this and other sections. Laminated beam theory and finite element analysis (FEA) were used to estimate the shear stiffness. Several references in the literature have hypothesized an increase in the effective measured shear stiffness due to warping. A third order laminated beam theory (TLBT) was derived to explore this concept, and the warping effect was found to be negligible. Furthermore, FEA results actually indicate a decrease in the effective shear stiffness at shorter spans for simple boundary conditions. This effect was attributed to transverse compression at the load points and supports. The higher order sandwich theory of Frostig shows promise for estimating the compression related error in the shear stiffness for thin-walled beams.

Part 2 attempts to identify the failure mechanism(s) under quasi-static loading and to develop a strength prediction for the DWB. FEA was utilized to investigate two possible failure modes in the top flange: compression failure of the carbon fiber plies and delamination at the free edges or taper regions. The onset of delamination was predicted using a strength-based approach, and the stress analysis was accomplished using a successive sub-modeling approach in ANSYS. The results of the delamination analyses were inconclusive, but the predicted strengths based on the compression failure mode show excellent agreement with the experimental data. A fatigue life prediction, assuming compression failure, was also developed using the remaining strength and critical element concepts of Reifsnider et al. One DWB fatigued at about 30% of the ultimate capacity showed no signs of damage after 4.9 million cycles, although the predicted number of cycles to failure was 4.4 million. A test on a second beam at about 60% of the ultimate capacity was incomplete at the time of publication. Thus, the success of the fatigue life prediction was not confirmed.

  Filename       Size       Approximate Download Time (Hours:Minutes:Seconds) 
 28.8 Modem   56K Modem   ISDN (64 Kb)   ISDN (128 Kb)   Higher-speed Access 
  Hayes_Appendix_A_TLBT.pdf 2.07 Mb 00:09:35 00:04:56 00:04:19 00:02:09 00:00:11
  Hayes_Appendix_B_ANSYS_code.pdf 47.55 Kb 00:00:13 00:00:06 00:00:05 00:00:02 < 00:00:01
  Hayes_Part_1_shear_stiffness.pdf 995.39 Kb 00:04:36 00:02:22 00:02:04 00:01:02 00:00:05
  Hayes_Part_2_strength_and_life_predictions.pdf 2.78 Mb 00:12:52 00:06:37 00:05:47 00:02:53 00:00:14

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