| タイトル | Combined investigation of Eddy current and ultrasonic techniques for composite materials NDE |
| 本文（外部サイト） | http://hdl.handle.net/2060/19950020358 |
| 著者（英） | Namkung, M.; Davis, C. W.; Nath, S.; Fulton, J. P. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1993-01-01 |
| 言語 | eng |
| 内容記述 | Advanced composites are not without trade-offs. Their increased designability brings an increase in the complexity of their internal geometry and, as a result, an increase in the number of failure modes associated with a defect. When two or more isotropic materials are combined in a composite, the isotropic material failure modes may also combine. In a laminate, matrix delamination, cracking and crazing, and voids and porosity, will often combine with fiber breakage, shattering, waviness, and separation to bring about ultimate structural failure. This combining of failure modes can result in defect boundaries of different sizes, corresponding to the failure of each structural component. This paper discusses a dual-technology NDE (Non Destructive Evaluation) (eddy current (EC) and ultrasonics (UT)) study of graphite/epoxy (gr/ep) laminate samples. Eddy current and ultrasonic raster (Cscan) imaging were used together to characterize the effects of mechanical impact damage, high temperature thermal damage and various types of inserts in gr/ep laminate samples of various stacking sequences. |
| NASA分類 | QUALITY ASSURANCE AND RELIABILITY |
| レポートNO | 95N26778
NASA-TM-110599
NAS 1.15:110599 |
| 権利 | No Copyright |
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