Composite Box Beam Analysis: Theory and Experiments

Abstract

Beam theory is widely used as a first approximation in numerous structural applica tions. When applied to composite beams, the accuracy of beam theory becomes ques tionable because (1) the shearing and warping deformations become significant, as the shearing stiffness of composite laminates is often very low, and (2) several elastic couplings can occur that strongly influence the behavior of composite beams. The tor sional behavior of thin-walled composite beams has important implications for aeronautical structures and is deeply modified by the above non-classical effects. This paper presents two comprehensive analysis methodologies for composite beams and describes experimental results obtained from a thin-walled, rectangular cross-sectional beam. The theoretical predictions are found in good agreement with the observed twist and strain distributions. Out-of-plane torsional warping of the cross-section is found to be the key factor for an accurate modeling of the torsional behavior of such structures.