The Proceedings of Conference of Tohoku Branch

Online ISSN : 2424-2713

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2002.37

Displaying 101-106 of 106 articles from this issue

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Analysis of Two way AGV Models

Yorimasa KUBA, Mitsuo YAMASHIRO

Article type: Article
Pages 198-199
Published: March 16, 2002
Released on J-STAGE: June 19, 2017

DOIhttps://doi.org/10.1299/jsmeth.2002.37.198

CONFERENCE PROCEEDINGS FREE ACCESS

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Fast inspection of internal defects of valve sleeves

Takashi GOMI, Masami MITO, Wei GAO, Satoshi KIYONO

Article type: Article
Pages 200-201
Published: March 16, 2002
Released on J-STAGE: June 19, 2017

DOIhttps://doi.org/10.1299/jsmeth.2002.37.200

CONFERENCE PROCEEDINGS FREE ACCESS

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Impact force identification of laminated composite plates using modal sensors

Takashi TAMURA, Hisao FUKUNAGA

Article type: Article
Pages 202-203
Published: March 16, 2002
Released on J-STAGE: June 19, 2017

DOIhttps://doi.org/10.1299/jsmeth.2002.37.202

CONFERENCE PROCEEDINGS FREE ACCESS

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Thermoelastic Analysis of Cracked Woven GFRP Laminates at Cryogenic Temperatures

Tomo TAKEDA, Yasuhide SHINDO, Fumio NARITA, Susumu KUMAGAI

Article type: Article
Pages 204-205
Published: March 16, 2002
Released on J-STAGE: June 19, 2017

DOIhttps://doi.org/10.1299/jsmeth.2002.37.204

CONFERENCE PROCEEDINGS FREE ACCESS

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We deal with the thermal-mechanical response of multi-layered G-11 woven glass/epoxy laminates with cracks and temperature-dependent properties under tension at liquid helium temperature (4K). The composite material is assumed to be in generalized plane strain. Cracks are located in the fill fiber bundles and are assumed to span the width of the fill fiber bundles. Finite element model is used to study the influence of residual thermal stresses on the mechanical behavior of multi-layered woven laminates with cracks. Numerical calculations are carried out, and the Young's modulus and stress distributions near the crack tip are shown graphically.

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Patching Efficiency in Cracked Plates Repaired with a Bonded Composite Patch Containing a Piezoelectric Fiber Composite Actuator Layer

Hideki SEKINE, Shinetsu FUJIMOTO, Tomomi HIRAI

Article type: Article
Pages 206-207
Published: March 16, 2002
Released on J-STAGE: June 19, 2017

DOIhttps://doi.org/10.1299/jsmeth.2002.37.206

CONFERENCE PROCEEDINGS FREE ACCESS

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Optimum Design of Composite Wing Considering Stiffened Panel Buckling

Yoko KATO, Ning HU, Masaki KAMEYAMA, Hisao FUKUNAGA

Article type: Article
Pages 208-209
Published: March 16, 2002
Released on J-STAGE: June 19, 2017

DOIhttps://doi.org/10.1299/jsmeth.2002.37.208

CONFERENCE PROCEEDINGS FREE ACCESS

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