| Autor: |
Knight, B., Howard, D. R., Ringermacher, H. I., Hudson, L. D. |
| Předmět: |
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| Zdroj: |
AIP Conference Proceedings; 2/22/2010, Vol. 1211 Issue 1, p466-473, 8p, 7 Diagrams, 1 Graph |
| Abstrakt: |
Infrared NDE techniques have proven to be superior for imaging of flaws in ceramic matrix composites (CMC) and carbon silicon carbide composites (C/SiC). Not only can one obtain accurate depth gauging of flaws such as delaminations and layered porosity in complex-shaped components such as airfoils and other aeronautical components, but also excellent reproducibility of image data is obtainable using the STTOF (Synthetic Thermal Time-of-Flight) methodology. The imaging of large complex shapes is fast and reliable. This methodology as applied to large C/SiC flight components at the NASA Dryden Flight Research Center will be described. [ABSTRACT FROM AUTHOR] |
| Databáze: |
Complementary Index |
| Externí odkaz: |
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