Pointwise energy release rate in delaminated plates
- 1 July 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 33 (7), 1312-1318
- https://doi.org/10.2514/3.12441
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Analysis of instability-related delamination growth using a crack tip elementAIAA Journal, 1993
- MIXED MODE ENERGY RELEASE RATE DETERMINATION FOR DELAMINATION BUCKLING USING A CRACK TIP ELEMENTPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- A METHOD FOR CALCULATING STRAIN ENERGY RELEASE RATE BASED ON BEAM THEORYPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- A Plate Finite Element for Modeling DelaminationsJournal of Reinforced Plastics and Composites, 1993
- A finite element for modeling delaminations in composite beamsComputers & Structures, 1991
- Dynamic Delamination Propagation in Composite BeamsJournal of Composite Materials, 1991
- A GLOBAL/LOCAL approach to lengthwise cracked beams: static analysisInternational Journal of Fracture, 1991
- Prediction of Energy Release Rate for Mixed-Mode Delamination Using Classical Plate TheoryApplied Mechanics Reviews, 1990
- Three-dimensional elastic analysis of a composite double cantilever beam specimenAIAA Journal, 1988
- A Path Independent Integral and the Approximate Analysis of Strain Concentration by Notches and CracksJournal of Applied Mechanics, 1968