Impact/fatigue performance of a (+/-45(sub 2), O(sub 4))(sub S) type carbon/epoxy laminate
By: W. G. J. 't Hart.
Contributors: National Aerospace Laboratory (The Netherlands)
Publisher: National Aerospace Laboratory
Published: 1985
Place of publication: Amsterdam
Number of pages: 31
Subjects: Aluminum; Compressive strength; Crack propagation; Epoxy matrix composites; Fatigue tests; Impact resistance; Laminates; Prepregs
Notes: Bibliographical references: p.12-14.