| タイトル | Evaluation of structural analysis methods for life prediction |
| 本文（外部サイト） | http://hdl.handle.net/2060/19880012127 |
| 著者（英） | Kaufman, A.; Saltsman, J. F.; Halford, G. R.; Tong, M. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1988-04-01 |
| 言語 | eng |
| 内容記述 | The utility of advanced constitutive models and structural analysis methods are evaluated for predicting the cyclic life of an air-cooled turbine blade for a gas turbine aircraft engine. Structural analysis methods of various levels of sophistication were exercised to obtain the cyclic stress-strain response at the critical airfoil location. Calculated strain ranges and mean stresses from the stress-strain cycles were used to predict crack initiation lives by using the total strain version of the strain range partitioning life prediction method. The major results are given and discussed. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 88N21511 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/146599 |
