Plane-Stress Fracture Toughness and Fatigue-Crack Propagation of Aluminum Alloy Wide Panels
- 1 January 1973
- book chapter
- Published by ASTM International
- p. 334-349
- https://doi.org/10.1520/stp49650s
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- EXPERIMENTAL PROGRAM TO DETERMINE EFFECT OF CRACK BUCKLING AND SPECIMEN DIMENSIONS ON FRACTURE TOUGHNESS OF THIN SHEET MATERIALSPublished by Defense Technical Information Center (DTIC) ,1966