dc.contributor.author | F.E. Keates | en_US |
dc.contributor.author | F.E. Kiddle | en_US |
dc.contributor.author | R.F. Mousley | en_US |
dc.contributor.author | D. Gunn | en_US |
dc.date.accessioned | 2014-10-21T15:51:33Z | |
dc.date.available | 2014-10-21T15:51:33Z | |
dc.date.issued | 1976 | en_US |
dc.identifier.other | ARC/R&M-3817 | en_US |
dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/3098 | |
dc.description.abstract | To assist the development and interpretation of the Concorde Major Fatigue Test a technique for accelerating fatigue testing was evaluated on structural box specimens under combined mechanical and thermal loadings. It is shown that for a moderate level of thermal fatigue the acceleration achieved was in reasonably good agreement with prediction but that at a high level of thermal fatigue the acceleration was appreciably higher than predicted. A tendency was observed for acceleration to be higher in crack propagation than in crack initiation. | en_US |
dc.relation.ispartofseries | Aeronautical Research Council Reports & Memoranda | en_US |
dc.title | Fatigue acceleration in box beams under mechanical and thermal stress (Second Series) | en_US |