Effects of Combined Mode Loadings on Fracture and Flaw Growth
- 1 September 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (9) , 1158-1164
- https://doi.org/10.2514/3.60523
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Crack growth and failure of aluminum plate under in-plane shearPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Propagation of a crack under general, in-plane tensionInternational Journal of Fracture, 1972
- Mode II Fatigue Crack PropagationJournal of Basic Engineering, 1971
- The effect of crack angle on fracture toughnessEngineering Fracture Mechanics, 1971
- On plane strain cyclic flaw growth ratesEngineering Fracture Mechanics, 1971
- Crack-Propagation Rate in 7075-T6 Plates Under Cyclic Tensile and Transverse Shear LoadingsJournal of Basic Engineering, 1969
- Application of Fracture Mechanics to Anisotropic PlatesJournal of Applied Mechanics, 1967
- On the Crack Extension in Plates Under Plane Loading and Transverse ShearJournal of Basic Engineering, 1963