{"created":"2023-06-20T15:15:17.114733+00:00","id":45359,"links":{},"metadata":{"_buckets":{"deposit":"f0c1a3e1-880e-4899-b915-abc801534f95"},"_deposit":{"created_by":1,"id":"45359","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45359"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045359","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["474341","474345","474343","474346","474340","474342","474339","474344"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Impact test of Carbon, Kevlar and Glass fibre hybrid FRP plates"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1991-04","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"18","bibliographicVolumeNumber":"1100","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1100","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"繊維及びプリプレグ(一方向とクロス)を変えた数種類のハイブリッドFRPを製作し,高速衝撃試験を行い繊維及びプリプレグの違いが耐衝撃性に与える影響について実験的に検討した。試験は高圧の窒素ガス銃を用いて80～280m/sの衝突速度で行った。試験片の支持条件は周辺固定である。飛翔体の衝突速度と残留速度はそれぞれ試験片の前後に置いた一対のフォトセンサーとカウンターを用いて計測した。同時に,0度と90度方向の衝撃歪応答も計測した。剥離領域面積は超音波深傷器を用いて測定した。損傷状態は吸収エネルギ量と剥離領域によって特徴づけられる。ハイブリッドFRPはガラス繊維を含むことにより耐衝撃性は向上する。また,耐衝撃性は一方向プリプレグ積層材の方がクロスプリプレグ積層材より有利であった。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The high velocity impact response of hybrid fiber reinforced plastic(FRP) plates(carbon, Kevlar and glass fibre) was experimentally studied to determine the influence of laminate structures. Impact velocities from 80-280 m/s were obtained using a high pressure nitrogen gas gun, with all the tested target specimens being mounted in a frame type fixture. The impact and residual velocities were measured by electronic counters connected to a system composed of two photo-cells and two infrared LEDs, and the tangential and radial direction dynamic strains were directly recorded. The delaminated area was subsequently measured by ultrasonic C-scanning, with the damage being characterized by this delaminated area and the energy-absorbing capacity.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1100000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-1100","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所原動機部"},{"subitem_text_value":"航空宇宙技術研究所原動機部"},{"subitem_text_value":"航空宇宙技術研究所構造力学部"},{"subitem_text_value":"石川島播磨重工業株式会社"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aeroengine Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Aeroengine Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Structural Mechanics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co., Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"橋本, 良作"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小河, 昭紀"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大竹, 邦彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"夏村, 匡"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HASHIMOTO, Ryosaku","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OGAWA, Akinori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OHTAKE, Kunihiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NATSUMURA, Tadashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-29"}],"displaytype":"detail","filename":"naltr01100.pdf","filesize":[{"value":"7.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01100.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45359/files/naltr01100.pdf"},"version_id":"21b9c4e1-fa80-46f8-866b-b94ad960782f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"impact test;  perforation;  damage;  hybrid FRP;  composite materials;  laminate structures","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"カーボン、ケブラー、ガラス系ハイブリッド複合材平板の衝撃試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"カーボン、ケブラー、ガラス系ハイブリッド複合材平板の衝撃試験"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"45359","relation_version_is_last":true,"title":["カーボン、ケブラー、ガラス系ハイブリッド複合材平板の衝撃試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:40:48.749048+00:00"}