Tension/Torsion Loading of Composite Laminates with Free-Edge Boundary Conditions

SM_STRUCT_1991-4454

10/29/1991

Authors
Abstract
Content

A finite element analysis of a family of quasi-isotropic graphite/epoxy laminates was conducted for tension, torsion, and combined tension/torsion loading. investigate The model was employed to the effects of delaminations on torsional stiffness and also to evaluate the total strain energy release rates associated with these delaminations.

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DOI
https://doi.org/10.4050/SM_STRUCT_1991-4454
Citation
Hooper, S., Hagemeier, R., and Ramaprasad, S., "Tension/Torsion Loading of Composite Laminates with Free-Edge Boundary Conditions," Rotorcraft Structures Technology for the 1990s and Beyond - Williamsburg, Virginia 1991, Williamsburg, Virginia, October 29, 1991, https://doi.org/10.4050/SM_STRUCT_1991-4454.
Additional Details
Publisher
Published
10/29/1991
Product Code
SM_STRUCT_1991-4454
Content Type
Technical Paper
Language
English