| タイトル | Measurement and analysis of critical CTOA for an aluminum alloy sheet |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940011475 |
| 著者（英） | Sutton, M. A.; Dawicke, D. S.; Newman, J. C., Jr.; Bigelow, C. A. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1993-09-01 |
| 言語 | eng |
| 内容記述 | The stable tearing behavior of thin sheets of 2024-T3 aluminum alloy was investigated for middle crack tension, M(T), and compact tension, C(T), specimens. The surface crack-tip opening angle (CTOA), applied loads, crack extension, and local displacements were measured. A critical CTOA fracture criterion was incorporated into a two-dimensional, elastic plastic finite element code and used to simulate the experimental fracture behavior. The CTOA measurements and observations of the fracture surfaces have shown that large values for surface CTOA were observed for small crack extensions (less than the sheet thickness); substantial tunneling of the crack was associated with small crack extensions; crack tunneling in the M(T) specimen was less than that observed in the C(T) configuration; for larger crack extensions, the measured CTOA values were determined to be approximately 6 degrees for both the M(T) and C(T) configuration; and for larger crack extensions, crack tunneling remained constant. The two-dimensional finite element predictions of fracture behavior assumed a constant critical CTOA value of 6 degrees and accounted for local crack tip constraint with a plane strain core of elements ahead of the crack tip. The plane strain core extended 5 mm above the crack plane. The simulations were within +/- 4 percent of the maximum applied load for the C(T) tests within 2 percent for the M(T) tests. |
| NASA分類 | METALLIC MATERIALS |
| レポートNO | 94N15948
NASA-TM-109024
NAS 1.15:109024 |
| 権利 | No Copyright |
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