Linking Riveting Process Parameters to the Fatigue Performance of Riveted Aircraft Structures
- 1 January 2000
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 37 (1) , 130-137
- https://doi.org/10.2514/2.2572
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Experimental Study of Fretting Crack Nucleation in Aerospace Alloys with Emphasis on Life PredictionPublished by ASTM International ,2000
- An integrated approach for prediction of fretting crack nucleation in riveted lap jointsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Shell Modeling of Fretting in Riveted Lap JointsAIAA Journal, 1998
- Fracture analysis of multi-site cracking in fuselage lap jointsComputational Mechanics, 1994
- FATIGUE DESIGN AND TEST PROGRAM FOR THE AMERICAN SSTPublished by Elsevier ,1972