| タイトル | Standard methods for open hole tension testing of textile composites |
| 本文（外部サイト） | http://hdl.handle.net/2060/19960012500 |
| 著者（英） | Portanova, M. A.; Masters, J. E. |
| 著者所属（英） | Lockheed Martin Engineering and Sciences Co. |
| 発行日 | 1995-12-01 |
| 言語 | eng |
| 内容記述 | Sizing effects have been investigated by comparing the open hole failure strengths of each of the four different braided architectures as a function of specimen thickness, hole diameter, and the ratio of specimen width to hole diameter. The data used to make these comparisons was primarily generated by Boeing. Direct comparisons of Boeing's results were made with experiments conducted at West Virginia University whenever possible. Indirect comparisons were made with test results for other 2-D braids and 3-D weaves tested by Boeing and Lockheed. In general, failure strength was found to decrease with increasing plate thickness, increase with decreasing hole size, and decreasing with decreasing width to diameter ratio. The interpretation of the sensitive to each of these geometrical parameters was complicated by scatter in the test data. For open hole tension testing of textile composites, the use of standard testing practices employed by industry, such as ASTM D5766 - Standard Test Method for Open Hole Tensile Strength of Polymer Matrix Composite Laminates should provide adequate results for material comparisons studies. |
| NASA分類 | COMPOSITE MATERIALS |
| レポートNO | 96N18737
NASA-CR-198262
NAS 1.26:198262
NIPS-96-08493 |
| 権利 | No Copyright |
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