NASA NTRS · 20000032296
Damage Detection and Impact Testing on Laminated and Sandwich Composite Panels
Abstract
This research investigates health monitoring of sandwich shell composites to determine if the Transmittance Functions (TF) are effective in determining the present of damage. The health monitoring test was conducted on the sandwich plates before and after low velocity impacts using the health monitoring technique given in TFs are a NDE (Nondestructive Evaluation) technique that utilizes the ratios of cross-spectrums to auto-spectrums between two response points on the sandwich composites. The test for transmittance was conducted on the same density foam core throughout the experiment. The test specimens were 17.8 cm by 25.4 cm in dimension. The external sheets (face sheets) were created from graphite/epoxy laminate with dimension of 1.58 mm thick. The polymethacrylide (Rohacell) foam core was 12.7 mm thick. These samples experienced a transformation in the TF that was considered the low velocity impact damage. The low velocity damage was observed in the TFs for the sandwich composites.
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Hughes, Derke R., Craft, William J., Schulz, Mark J., Naser, Ahmad S., Martin, William N.. 1998-02-22. Damage Detection and Impact Testing on Laminated and Sandwich Composite Panels. https://ntrs.nasa.gov/citations/20000032296
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