High Performance Composites: Proceedings, Canadian Fracture Conference 8, Millcroft Inn, Alton, Ontario, October 7 & 8, 1982 |
Contents
Effect of Interlaminar Flaws on the Compressive | 16 |
Critical Properties for Fibre Composite High | 28 |
FRACTURE AND FATIGUE | 38 |
Copyright | |
5 other sections not shown
Common terms and phrases
analysis ANGLE application AS-CARBON axial beam BIAXIAL Canada carbon carbon fibre cement chamber compared Composite Materials compressive controlled cost crack curve cycles detailed determined diameter direction effect energy energy density Engineering epoxy equation EXPERIMENTAL fabricated factor failure fatigue fibers fibre composites Figure flat bar Flaw flywheel fracture function geometry given glass higher impact increase Kevlar 49 laminates levels limit lines loading longitudinal machine matrix measured Mechanical metals method modulus obtained occurs outer plane plotted polymer predicted presented pressure properties pulp RADIAL range ratio reinforced relative resin ring rotor S2-GLASS shear strength shear stress sheet shown shows shrinkage solutes specimens strain stress structural surface Table TANGENTIAL technique temperature tensile strength tension tests thick torsional toughness transverse University values volume fraction weight winding wood woven