Residual properties of notched [0/90]4S AS4/PEEK composite laminates after fatigue and re-consolidation
Authors:
- C.M WangCWC.M Wang
- C.S ShinC.S Shin
- 1 January 2002
- journal article
- Published by Elsevier in Composites Part B: Engineering
- Vol. 33 (1) , 67-76
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Effects of hole machining defects on strength and fatigue life of composite laminatesComposites Part A: Applied Science and Manufacturing, 1997
- Recycling Carbon-Fiber-Reinforced Thermoplastic CompositesJournal of Thermoplastic Composite Materials, 1996
- Effect of Cooling Rate and Stacking Sequence on the Fatigue Behavior of Notched Quasi-Isotropic AS4/PEEK LaminatesJournal of Composites Technology and Research, 1996
- Damage and Residual Properties of Notched [0/± 45/90]s and [0/90]2s Graphite/PEEK Woven Laminates Under Reversed FatigueJournal of Thermoplastic Composite Materials, 1994
- Damage mechanics of composite materials: I— Measurements of damage and strengthComposites Science and Technology, 1990
- The elasticity and strength of paper and other fibrous materialsBritish Journal of Applied Physics, 1952