You need JavaScript to view this

Evaluation of test specimen shape effects on the flexural fatigue of CFRP laminates; Chokko sekiso CFRP no mage tsukare shiken ni okeru shikenhen keijo no hyoka ni kansuru kenkyu

Abstract

An investigation was made on relationship between a flexural fatigue test and test specimen shapes of carbon fiber reinforced plastic (CFRP). Five kinds of material were tested including carbon fibers with medium strength, high ductility, and high strength, cross-ply laminates as pre-preg base materials using epoxy resin for raw material, and pseudo isotropic laminates. Static bending test and flexural fatigue test were carried out for dynamic characteristics to derive the relationship (S-N line) between iterative bending stress and the number of repetition before breakdown. Comparison of the test results arrived at the following conclusions: The high-ductility and high-strength laminates exhibited significant difference in the S-N inclination, which is because of local compression breakdown at edges of the laminates; the flexural fatigue strength is compared in a descending order as the medium-strength laminates, high-ductility laminates, high-strength laminates, high-strength pseudo isotropic laminates, and medium-strength fabric laminates. The static bending strength was in the order of the high-strength laminates, high-ductility laminates, high-strength pseudo isotropic laminates, and medium-strength fabric laminates. 12 refs., 16 figs., 2 tabs.
Authors:
Noguchi, Y [1] 
  1. National Aerospace Laboratory, Tokyo (Japan)
Publication Date:
May 01, 1992
Product Type:
Technical Report
Report Number:
NAL-TR-1159
Reference Number:
SCA: 360603; PA: NEDO-93:930017; SN: 93000997996
Resource Relation:
Other Information: PBD: May 1992
Subject:
36 MATERIALS SCIENCE; LAYERS; CONFIGURATION; REINFORCED PLASTICS; CARBON FIBERS; MECHANICAL TESTS; FATIGUE; BENDING; SAMPLE PREPARATION; SHAPE; STRESSES; FRACTURES; S-N DIAGRAM; ELONGATION; FRACTURE PROPERTIES; COMPRESSION; TEXTILES; 360603; MECHANICAL PROPERTIES
OSTI ID:
10156030
Research Organizations:
National Aerospace Lab., Chofu, Tokyo (Japan)
Country of Origin:
Japan
Language:
Japanese
Other Identifying Numbers:
Other: ON: DE93793622; TRN: 93:930017
Availability:
OSTI; NTIS; Available from National Aerospace Laboratory, 44-1, Shindaiji Higashicho 7-chome, Chofu-City, Tokyo, Japan
Submitting Site:
NEDO
Size:
17 p.
Announcement Date:
Jul 06, 2005

Citation Formats

Noguchi, Y. Evaluation of test specimen shape effects on the flexural fatigue of CFRP laminates; Chokko sekiso CFRP no mage tsukare shiken ni okeru shikenhen keijo no hyoka ni kansuru kenkyu. Japan: N. p., 1992. Web.
Noguchi, Y. Evaluation of test specimen shape effects on the flexural fatigue of CFRP laminates; Chokko sekiso CFRP no mage tsukare shiken ni okeru shikenhen keijo no hyoka ni kansuru kenkyu. Japan.
Noguchi, Y. 1992. "Evaluation of test specimen shape effects on the flexural fatigue of CFRP laminates; Chokko sekiso CFRP no mage tsukare shiken ni okeru shikenhen keijo no hyoka ni kansuru kenkyu." Japan.
@misc{etde_10156030,
title = {Evaluation of test specimen shape effects on the flexural fatigue of CFRP laminates; Chokko sekiso CFRP no mage tsukare shiken ni okeru shikenhen keijo no hyoka ni kansuru kenkyu}
author = {Noguchi, Y}
abstractNote = {An investigation was made on relationship between a flexural fatigue test and test specimen shapes of carbon fiber reinforced plastic (CFRP). Five kinds of material were tested including carbon fibers with medium strength, high ductility, and high strength, cross-ply laminates as pre-preg base materials using epoxy resin for raw material, and pseudo isotropic laminates. Static bending test and flexural fatigue test were carried out for dynamic characteristics to derive the relationship (S-N line) between iterative bending stress and the number of repetition before breakdown. Comparison of the test results arrived at the following conclusions: The high-ductility and high-strength laminates exhibited significant difference in the S-N inclination, which is because of local compression breakdown at edges of the laminates; the flexural fatigue strength is compared in a descending order as the medium-strength laminates, high-ductility laminates, high-strength laminates, high-strength pseudo isotropic laminates, and medium-strength fabric laminates. The static bending strength was in the order of the high-strength laminates, high-ductility laminates, high-strength pseudo isotropic laminates, and medium-strength fabric laminates. 12 refs., 16 figs., 2 tabs.}
place = {Japan}
year = {1992}
month = {May}
}