Compression Behavior of A= 45 -Dominated Laminates with a Circular Hole or Impact Damage
- 1 January 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 24 (1), 115-122
- https://doi.org/10.2514/3.48652
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
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- Strength Predictions of Composite Laminates with Unloaded Fastener HolesAIAA Journal, 1980
- The fracture behavior of graphite/epoxy laminatesExperimental Mechanics, 1979
- Failure Modes of Angle Ply LaminatesJournal of Composite Materials, 1975
- Effects of material and stacking sequence on behavior of composite plates with holesExperimental Mechanics, 1974