journal article·2022-06

Prediction of the spring-in of cylindrically orthotropic media and cross-ply laminates

R Byron Pipes, Kwanchai Chinwicharnam, Eduardo Barocio

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Abstract

The equation for prediction of the spring-in angle of a cylindrically orthotropic segment is shown to be independent of all material properties except for the anisotropic coefficients of thermal expansion and a stress-free state is insured for the corresponding unconstrained deformation. In contrast, the complete cylindrical geometry is shown to provide constraint to thermal deformation and thereby induce thermal residual stresses in the form of a moment. The method of superposition is demonstrated whereby traction-free conditions yield stress-free cylindrical elements with corresponding angular displacements at the element free boundaries. The first derivation of the spring-in equation is attributed to Radford, in contrast to the widely accepted view that the equation was first developed by Spencer et al. Finite-element methods, combined with the superposition approach, further validate the accuracy of the Radford equation for cylindrically orthotropic segments and explore its limitations for multiaxial composite laminates.
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Research context

OpenAlex topics: Composite Structure Analysis and Optimization · Epoxy Resin Curing Processes · Mechanical Behavior of Composites

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

CMSC, Purdue University, West Lafayette, IN, USA

Aeronautics and Astronautics, Purdue University, West Lafayette, IN, USA

References (9)

Show source-provided references
1. Radford W · 1987
2. Lekhnitskii SG · 1981
3. Çiçek kF · 2014
4. O’Neill JM · Math Engng Ind · 1988 · 2 · 65
5. ABAQUS, https://www.3ds.com/products-services/simulia/products/abaqus/
6. 10.1016/S1359-8368(02)00002-110.1016/S1359-8368(02)00002-1 ↗
7. 10.1177/073168440934070710.1177/0731684409340707 ↗
8. 10.1177/07316844930120010410.1177/073168449301200104 ↗
9. 10.1016/0961-9526(95)00033-J10.1016/0961-9526(95)00033-J ↗