Engineering Papers⌕ Search

NASA NTRS · 19920068890

Compression-after-impact testing of thin composite materials

Abstract

A new method has been devised to test composite specimens as thin as 8 plies and up to 7.6 cm in width for compression strength. This method utilizes a fixture incorporating the best features of the Celanese and IITRI fixtures combined with an antibuckling jig developed at the University of Dayton Research Institute. This new method uses up to 83 percent less material than the most commonly used compression-after-impact technique (which calls for a 48 ply test specimen) and can also be performed on smaller loading frames since a much smaller force is needed to fail the specimen. The thickness of the test specimen can be fabricated to exactly match production part thickness, thus yielding more meaningful results. CAI tests were performed on IM6/3501 carbon/epoxy utilizing this new method. To verify the design, a series of tests were performed in which undamaged specimens were tested using the new fixture and ASTM D 3410-87 (Celanese compression test) and the results compared. The new fixture works well and will be a valuable asset to MSFC's damage tolerance program.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Nettles, Alan T., Hodge, Andrew J.. 1991-01-01. Compression-after-impact testing of thin composite materials. https://ntrs.nasa.gov/citations/19920068890

Cite the original work for its findings. Save a collection to share your selection of sources.