| タイトル | Numerical Strip-Yield Calculation of CTOD |
| 本文（外部サイト） | http://hdl.handle.net/2060/20070017318 |
| 著者（英） | Forman, Royce; Beek, Joachim |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 2007-04-16 |
| 言語 | eng |
| 内容記述 | Many existing methods to calculate CTOD can be costly and complicated, or apply only to particular configurations. A new numerical method for calculating CTOD was investigated. NASGRO's Boundary Element module NASBEM was adapted to calculate displacements at any point on the crack. Demonstrated for a number of crack configurations: a) finite and infinite domains; b) center and edge cracks; and c) complex cases with several cracks and holes. Great accuracy at minimal computational cost. |
| NASA分類 | Aircraft Design, Testing and Performance |
| 権利 | No Copyright |
