An Analytical Investigation of the Trapeze Effect Acting on a Thin Flexible Ribbon

Author:

Sicard Jérôme F.1,Sirohi Jayant2

Affiliation:

1. Department of Aerospace Engineering and Engineering Mechanics, The University of Texas at Austin, Austin, TX 78712 e-mail:

2. Associate Professor Department of Aerospace Engineering and Engineering Mechanics, The University of Texas at Austin, Austin, TX 78712 e-mail:

Abstract

This paper systematically explores the extensional–torsional coupling due to the trapeze effect acting on a thin flexible ribbon subjected to combined tension and torsion. Kinematic relationships as well as expressions for the restoring torque associated with this effect are analytically derived. Additionally, the locus of points about which the cross sections of a twisted ribbon under tension rotate is derived. These points, called torsional centers, are found to be coincident with the centroids of the axial stress field at each station along the ribbon. More generally, it is shown that when a flexible slender member is in tension, combined transverse forces must act at the centroid of the axial stress field to produce pure bending and no twist. As a result, the elastic axis (EA) of the member shifts from the locus of shear centers to the locus of centroids of the axial stress field. A numerical model is developed to investigate the effect of the position of the EA on the prediction of steady-state deformations and natural frequencies of a rotating ribbon with tip mass. By assuming the EA to be the locus of the shear centers, the tip twist is overpredicted by a factor of 2 for small twist angles, and up to 2.5 for large twist deformations. In addition, assuming the EA to be the locus of shear centers results in an error of up to 60% in the predicted natural frequencies at large twist angles.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference19 articles.

1. On Vibration Galvanometer With Unifilar Torsional Control;Proc. Phys. Soc. London,1911

2. On an Anomalous Variation of the Rigidity of Phosphor Bronze;Philos. Mag. Ser. 6,1913

3. The Bifilar Property of Twisted Strips;Philos. Mag. Ser. 6,1914

4. Houbolt, J. C., and Brooks, G. W., 1957, “Differential Equations of Motion for Combined Flapwise Bending, Chordwise Bending, and Torsion of Twisted Nonuniform Rotor Blades,” Langley Aeronautical Laboratory, National Advisory Committee for Aeronautics, Langley Field, VA, Technical Note No. 3905.

5. Aeroelastic Stability of Composite Hingeless Rotor Blades in Hover—Part I: Theory;Math. Comput. Modell.,1993

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