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Volume 13 (1987)
- Issue 6 Pages 251-
- Issue 5 Pages 203-
- Issue 4 Pages 151-
- Issue 3 Pages 99-
- Issue 2 Pages 51-
- Issue 1 Pages 1-
Volume 13, Issue 4
Displaying 1-8 of 8 articles from this issue
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Yuzuru KAMATA, Keiji FUKUSHI, Matao NAGAI1987 Volume 13 Issue 4 Pages 151-156
Published: July 15, 1987
Released on J-STAGE: August 11, 2009
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Takashi KOSAKA1987 Volume 13 Issue 4 Pages 156-162
Published: July 15, 1987
Released on J-STAGE: August 11, 2009
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[in Japanese]1987 Volume 13 Issue 4 Pages 162a
Published: July 15, 1987
Released on J-STAGE: August 11, 2009
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A Study of Secondary Operation of FRMY. TADA, T. SATO1987 Volume 13 Issue 4 Pages 163-168
Published: July 15, 1987
Released on J-STAGE: August 11, 2009
JOURNAL FREE ACCESSThe plane strain compression behavior and change in mechanical properties of aluminum composite reinforced with SiC fiber have been examined. The load required for the plane strain compression was estimated with an upper bound technique and showed good agreement with experiments. During the compression tests, any fracture or cracking of specimens did not occur in the range of 60% reduction in height. Tensile strengths of the specimens decreased rapidly with the increase of the reduction; for example, 20% fall in strength after 10% reduc-tion. The modulus of elasticity, however, remained constant. It was suggested that the decrease in tensile strength was a result of disorder in fiber alignment and/or void formation at matrix/fiber interface.View full abstractDownload PDF (3539K) -
H. IYAMA, M. NOMOTO, Y. HIRANO1987 Volume 13 Issue 4 Pages 169-179
Published: July 15, 1987
Released on J-STAGE: August 11, 2009
JOURNAL FREE ACCESSLaminate configurations of some composite plates for practical use can be considered to be quasi-orthotropic. In the present paper experimental results on tensile strength of laminates with loaded and unloaded circular holes are described. The plates are made of carbon fibre reinforced plastics and can be considered to be either quasi-isotropic or quasi-orthotropic. The experimental results are compared with the calculated first failure strength. The calculations are made by applying Lekhnitskii's stress expression for orthotropic plates with circular holes and Zhang and Ueng's approximate stress expression for orthotropic plates with pin-loaded holes. The calculated strength is much lower than the experimental one as expected. Some consideration about the discrepancy is given.View full abstractDownload PDF (5770K) -
Zenichiro MAEKAWA1987 Volume 13 Issue 4 Pages 180-188
Published: July 15, 1987
Released on J-STAGE: August 11, 2009
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Tsuyoshi HAYASHI1987 Volume 13 Issue 4 Pages 189-194
Published: July 15, 1987
Released on J-STAGE: August 11, 2009
JOURNAL FREE ACCESSDownload PDF (670K) -
1987 Volume 13 Issue 4 Pages 195-197
Published: July 15, 1987
Released on J-STAGE: February 08, 2010
JOURNAL FREE ACCESSDownload PDF (461K)
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