Journal of the Japan Society for Composite Materials

Online ISSN : 1884-8559
Print ISSN : 0385-2563
ISSN-L : 0385-2563

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Volume 10, Issue 3

Displaying 1-10 of 10 articles from this issue

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[title in Japanese]

Isao KIMPARA

1984 Volume 10 Issue 3 Pages 97-101
Published: July 31, 1984
Released on J-STAGE: August 11, 2009

DOIhttps://doi.org/10.6089/jscm.10.97

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[title in Japanese]

[in Japanese]

1984 Volume 10 Issue 3 Pages 101a
Published: July 31, 1984
Released on J-STAGE: August 11, 2009

DOIhttps://doi.org/10.6089/jscm.10.101a

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[title in Japanese]

Hiromitsu OHTSUKA

1984 Volume 10 Issue 3 Pages 102-106
Published: July 31, 1984
Released on J-STAGE: August 11, 2009

DOIhttps://doi.org/10.6089/jscm.10.102

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[title in Japanese]

Kei URABE

1984 Volume 10 Issue 3 Pages 107-110
Published: July 31, 1984
Released on J-STAGE: August 11, 2009

DOIhttps://doi.org/10.6089/jscm.10.107

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[title in Japanese]

Yujiro YOSHIDA, Tosio SAKAKIBARA

1984 Volume 10 Issue 3 Pages 111-115
Published: July 31, 1984
Released on J-STAGE: August 11, 2009

DOIhttps://doi.org/10.6089/jscm.10.111

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[title in Japanese]

Kazuyoshi NINOMIYA, Akira AIKAWA, Makoto OISHIBASHI, Takao MANIWA

1984 Volume 10 Issue 3 Pages 116-121
Published: July 31, 1984
Released on J-STAGE: August 11, 2009

DOIhttps://doi.org/10.6089/jscm.10.116

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[title in Japanese]

Takahito HOSOKAWA, Masaatsu HOSOYA

1984 Volume 10 Issue 3 Pages 122-126
Published: July 31, 1984
Released on J-STAGE: August 11, 2009

DOIhttps://doi.org/10.6089/jscm.10.122

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In-plane Shear Properties of Fabric-CFRP/Aluminum-Honeycomb Sandwich Panels

Y. NOGUCHI, T. FURUTA

1984 Volume 10 Issue 3 Pages 127-131
Published: July 31, 1984
Released on J-STAGE: August 11, 2009

DOIhttps://doi.org/10.6089/jscm.10.127

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The objective of this paper is to evaluate the in-plane shear properties of honeycomb sandwich panel with face members of fabric CFRP. The face members was made of two plies, 8-harness-satin CFRP laminated with ±45° orientation angles. The elastic constants and in-plane shear strength of the CFRP face members were calculated theoretically. Three test specimens of sandwich panel were loaded in shear by the applied tensile load in the diagonal direction at the opposite corners of a rhombic test frame. The calculated results reasonably predicted the test results.

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[title in Japanese]

Isao KIMPARA

1984 Volume 10 Issue 3 Pages 132
Published: July 31, 1984
Released on J-STAGE: August 11, 2009

DOIhttps://doi.org/10.6089/jscm.10.132

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[title in Japanese]

1984 Volume 10 Issue 3 Pages 133-137
Published: July 31, 1984
Released on J-STAGE: February 08, 2010

DOIhttps://doi.org/10.6089/jscm.10.133

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