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モアレ法による薄い複合材料のひずみ解析
https://jaxa.repo.nii.ac.jp/records/45012
https://jaxa.repo.nii.ac.jp/records/45012cb2d37ec-d6d0-4509-b5dc-d0caa983f28b
名前 / ファイル | ライセンス | アクション |
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naltr00754.pdf (4.0 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | モアレ法による薄い複合材料のひずみ解析 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Strain Analysis of Thin Composites with Moire Method | |||||
著者 |
越出, 慎一
× 越出, 慎一× 高松, 英男× 長崎, 守高× KOSHIDE, Shinichi× TAKAMATSU, Hideo× NAGASAKI, Moritaka |
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著者所属 | ||||||
航空宇宙技術研究所機体第二部 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属(英) | ||||||
en | ||||||
Second Airframe Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan(NASDA) | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan(NASDA) | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-754 巻 754, p. 14, 発行日 1983-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The paper describes the strain analysis of ultra-thin composites by the moire method. A technique for printing moire grating on the surface of ultra-thin materials and a testing procedure to accurately measure the strain on such materials, are contrived. The specimen gratings are recorded on the films by taking photographs of specimens under testing with the testing procedure. Moire fringe patterns from underformed gratings and deformed gratings are observed by inserting the films into the optical spatial filtering system with coherent light. The differences between the fringe patterns depend on only in-plane displacement. Strain components are determined from the differences. The method was applied to strain analysis for tensile tests and creep tests of two kinds of thin materials which were manufactured for trial use in balloon satellite structures. The materials are thin polyestel sheets reinforced with glass fiber cloth and thin composites consisting of polyethylene terephtalate film sandwiched between two layers of aluminum foil. The results of these tests indicated that the method was applicable to strain analysis and flaw detection in ultra-thin materials. Moreover, the mechanical properties of these thin composites were clarified with these tests. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0754000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-754 |