Initiation and Growth of Fatigue Cracks in and Residual Strength of the F-100 Wing
- 1 January 1971
- book chapter
- Published by ASTM International
- p. 144-163
- https://doi.org/10.1520/stp26677s
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Stress Analysis of CracksPublished by ASTM International ,1965
- Applied Fracture MechanicsPublished by ASTM International ,1965