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Compression After Impact Strength Comparison of Rohacell Foam and Aluminum Honeycomb Core Sandwich StructureThis Technical Memorandum is a follow-on study to a previous one1 that examined the compression after impact (CAI) strength of carbon fiber sandwich structure with aluminum honeycomb core and Rohacell foam core with barely visible impact damage (BVID). In this current study a wider range of impact energies were utilized and the CAI strength assessed with these different damage severity levels. This was done to provide a more complete database for the two types of sandwich structure tested in these studies. In addition, the honeycomb sandwich specimens were tested with both the ‘L’ and ‘W’ directions aligned with the axis of compression loading. As in the study examining CAI strength with BVID1, the results were normalized by the mass of the sandwich structure. The results showed that the CAI strength did differ depending on the orientation of the core during testing and that when tested in the W-direction, the honeycomb core sandwich structure had about the same CAI strength as the foam core sandwich structure when normalized by the mass of the sandwich structures.
Document ID
20210016152
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
A T Nettles
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
May 24, 2021
Publication Date
May 1, 2021
Publication Information
Subject Category
Composite Materials
Report/Patent Number
M-1524
NASA/TM-20210016152
Funding Number(s)
WBS: 585777.08.50.50.40.14
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Sandwich Structure
Rohacel®
honeycomb
damage tolerance
impact damage
carbon fiber
compression after impact (CAI)
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