Compression of Thick Laminated Composite Beams with Initial Impact-Like Damage

By: Nasa, National Aeronautics and Space Adm

While the study of compression after impact of laminated composites has been under consideration for many years, the complexity of the damage initiated by low velocity impact has not lent itself to simple predictive models for compression strength. The damage modes due to non-penetrating, low velocity impact by large diameter objects can be simulated using quasi-static three-point bending. The resulting damage modes are less coupled and more easily characterized than actual impact damage modes. This study includes the compression testing of specimens with well documented initial damage states obtained from three-point bend testing. Compression strengths and failure modes were obtained for quasi-isotropic stacking sequences from 0.24 to 1.1 inches thick with both grouped and interspersed ply stacking. Initial damage prior to compression testing was divided into four classifications based on the type, extent, and location of the damage. These classifications are multiple through-thickness delaminations, isolated delamination, damage near the surface, and matrix cracks. Specimens from each classification were compared to specimens tested without initial damage in order to determine the effects of the initial damage on the final compression strength and failure modes. A finite element analysis was used to aid in the understanding and explanation of the experimental results. Breivik, N. L. and Guerdal, Z. and Griffin, O. H., Jr. BEAMS (SUPPORTS); BENDING; COMPRESSION LOADS; DELAMINATING; IMPACT DAMAGE; LAMINATES; PERFORMANCE PREDICTION; COMPRESSIVE STRENGTH; FAILURE MODES; FINITE ELEMENT METHOD; LOW SPEED; SURFACE CRACKS...

• Format: Paperback
• Language: English
• ISBN: 1731530501
• ISBN13: 9781731530509
• Release Date: January 1
• Publisher: Independently Published
• Length: 178 Pages
• Weight: 0.94 lbs.
• Dimensions: 0.4" x 8.5" x 11.0"