Specimen Design for Sustained Load Testing of Parallel-Laid Glass Fibre Reinforced Plastics.

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Abstract:

The specimen adopted and recommended is prepared by making three laminates, two of them to form the reinforcing end pieces and the third for the test piece. The three laminates are then bonded together in a mold using single layers of prepreg as bonding agent. The bonding surfaces are specially prepared by molding on a sheet of woven glass fabric and stripping this off just before bonding, to leave a roughened surface. The test specimens are 12 inch wide strips cut from the laminates. Author, modified-PL

Author(s):
Berry, D. B. S. ; Farley, P. R.
Author Organization(s):
DIRECTORATE OF MATERIALS AVIATION LONDON (ENGLAND)
Descriptive Note:
Rept. for Sep 67-May 70,
Pagination:
0015

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
D-MAT-172, TRC-BR-23590
Monitor Series:
BR-23590
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*REINFORCED PLASTICS, LOADS(FORCES), EPOXY RESINS, UNITED KINGDOM
Field(s)/Group(s):
Laminates and Composite Materials
Keyword(s):
FIBER COMPOSITES, *FIBERGLASS REINFORCED PLASTICS, EPOXY MATRIX COMPOSITES
Report Date:
1970 Aug 01