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The Role of Brittle Lacquer Techniques in the Strength-test of FRP Joints
https://jaxa.repo.nii.ac.jp/records/44882
https://jaxa.repo.nii.ac.jp/records/4488228d24b71-cb1a-465c-a1dc-9c1a36910973
名前 / ファイル | ライセンス | アクション |
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naltr00627.pdf (3.2 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 | ||||||
言語 | en | |||||
タイトル | The Role of Brittle Lacquer Techniques in the Strength-test of FRP Joints | |||||
言語 | ||||||
言語 | eng | |||||
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 | ||||||
その他のタイトル | 応力塗料を用いたFRP円筒結合部の強度試験 | |||||
著者 |
野原, 利雄
× 野原, 利雄× 江川, 幸一× 野口, 義男× NOHARA, Toshio× EGAWA, Koichi× NOGUCHI, Yoshio |
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著者所属 | ||||||
航空宇宙技術研究所機体第一部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所機体第一部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所機体第一部 | ||||||
著者所属(英) | ||||||
en | ||||||
First Airframe Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
First Airframe Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
First Airframe Division, National Aerospace Laboratory(NAL) | ||||||
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-627 巻 627, p. 21, 発行日 1980-09 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A brittle lacquer mapping technique was used to check the strength of the jointed part of a composite F.W. cylinder. The test was done by using the following steps; 1)By using the results from the analysis and the bending test of specimens made from the same kind of composite F.W. cylinder, the brittle lacquer map of fracture and the map on the location of sufficient strength in the specimen were found. 2)Comparing these two maps with the brittle lacquer mapping on the test structure, a search was made to find fractures, cracks around holes and stress concentrated areas of the test structure, especially its jointed part. The test structure, NAL-7P one stage rocket, was bent by the 15G load applied in the center of its joint. There were not any fractures or cracks in the test structure, but a few stress concentrated and hoop stressed areas were found. | |||||
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: NALTR0627000 | |||||
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-627 |