An integrated approach for prediction of fretting crack nucleation in riveted lap joints
- 12 April 1999
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Linking riveting process parameters to the fatigue performance of riveted aircraft structuresPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Observation, analysis and prediction of fretting fatigue in 2024-T351 aluminum alloyWear, 1998
- Shell Modeling of Fretting in Riveted Lap JointsAIAA Journal, 1998
- Mechanics of fretting fatigue crack formationWear, 1996
- Analysis of fretting conditions in pinned connectionsWear, 1995
- An analysis of fretting-fatigue failure combined with numerical calculations to predict crack nucleationWear, 1995
- An analysis of fretting-fatigue failure combined with numerical calculations to predict crack nucleationWear, 1995