NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The effects of specimen scale on the compression strength of composite materialsThis paper presents a number of observations on the effect of specimen scale on the compression response of composite materials. Work on this topic was motivated by observations that thick-walled, unstiffened carbon reinforced cylinders subjected to hydrostatic pressure were not reaching inplane laminate stress levels at failure expected from coupon level properties, while similar cylinders reinforced with fiberglass were. Results from a study on coupon strength of (0/0/90) laminates, reinforced with AS4 carbon fiber and S2 glass fiber, are presented and show that compression strength is not a function of material or specimen thickness for materials that have the same laminate quality (autoclave cured quality). Actual laminate compression strength was observed to decrease with increasing thickness, but this is attributed to fixture restraint effects on coupon response. The hypothesis drawn from the coupon level results is further supported by results from a compression test on a thick carbon reinforced coupon in a fixture with reduced influence on specimen response and from a hydrostatic test on an unstiffened carbon reinforced cylinder subjected to hydrostatic pressure with end closures designed to minimize their effect on cylinder response.
Document ID
19940033291
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Camponeschi, Eugene Thomas, Jr.
(Naval Surface Warfare Center Annapolis, MD, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Publication Information
Publication: NASA. Langley Research Center, Workshop on Scaling Effects in Composite Materials and Structures
Subject Category
Structural Mechanics
Accession Number
94N37802
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available