WEKO3
アイテム
{"_buckets": {"deposit": "2eff71af-dfe3-4bd4-83cb-f0f743c83235"}, "_deposit": {"created_by": 1, "id": "36823", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "36823"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00036823", "sets": ["1891", "1915"]}, "author_link": ["425003", "425006", "425009", "425005", "425010", "425004", "425008", "425007"], "item_5_alternative_title_1": {"attribute_name": "その他のタイトル", "attribute_value_mlt": [{"subitem_alternative_title": "革新航空機要素技術についての政府産業界特別共同研究"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1996-05", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "168", "bibliographicPageStart": "1", "bibliographicVolumeNumber": "31", "bibliographic_titles": [{"bibliographic_title": "航空宇宙技術研究所特別資料"}, {"bibliographic_title": "Special Publication of National Aerospace Laboratory", "bibliographic_titleLang": "en"}]}]}, "item_5_description_16": {"attribute_name": "抄録", "attribute_value_mlt": [{"subitem_description": "以下の主題について論じた。オイル流れの可視化、抗力測定、3次元境界層遷移、圧縮性境界層、超音速層流制御、圧縮性層流制御、ファスナー接合要素解析、ファスナー接合構造要素における熱伝導、流体と構造物間の熱伝達、超音速機用軽金属材料、超音速機用繊維/金属ラミネート、耐損傷胴体構造解析、炭素繊維強化プラスチック複合部材の非破壊評価、T字型補強部材の座屈、および補強部材の表皮剥離。", "subitem_description_type": "Abstract"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "The following topics were discussed: oil flow visualization, drag measurement, three dimensional boundary layer transition, compressible boundary layers, supersonic laminar flow control, compressible laminar flow control, fastener jointed component analysis, heat conduction in fastener jointed structural components, thermal transfer between fluid and structure, light metallic materials for supersonic transport, fiber/metal laminates for supersonic transport, damage tolerant fuselage structure analysis, nondestructive evaluation for carbon fiber reinforced plastic composites member, buckling of T-shaped stiffener, and skin disbond of stiffener.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0000440000", "subitem_description_type": "Other"}]}, "item_5_description_33": {"attribute_name": "レポート番号", "attribute_value_mlt": [{"subitem_description": "レポート番号: NAL SP-31", "subitem_description_type": "Other"}]}, "item_5_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "航空宇宙技術研究所"}]}, "item_5_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "National Aerospace Laboratory (NAL)"}]}, "item_5_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0289-260X", "subitem_source_identifier_type": "ISSN"}]}, "item_5_source_id_24": {"attribute_name": "書誌レコードID", "attribute_value_mlt": [{"subitem_source_identifier": "AN10097345", "subitem_source_identifier_type": "NCID"}]}, "item_5_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 航空宇宙技術研究所"}]}, "item_5_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: AP"}]}, "item_5_text_43": {"attribute_name": "DSpaceコレクション番号", "attribute_value_mlt": [{"subitem_text_value": "DSpaceコレクション番号: 7"}]}, "item_5_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "航空宇宙技術研究所"}, {"subitem_text_value": "三菱重工業"}, {"subitem_text_value": "川崎重工業"}, {"subitem_text_value": "富士重工業"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "National Aerospace Laboratory"}, {"subitem_text_language": "en", "subitem_text_value": "Mitsubishi Heavy Industries, Ltd"}, {"subitem_text_language": "en", "subitem_text_value": "Kawasaki Heavy Industries, Ltd"}, {"subitem_text_language": "en", "subitem_text_value": "Fuji Heavy Industries, Ltd"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "航空宇宙技術研究所"}], "nameIdentifiers": [{"nameIdentifier": "425003", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "三菱重工業"}], "nameIdentifiers": [{"nameIdentifier": "425004", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "川崎重工業"}], "nameIdentifiers": [{"nameIdentifier": "425005", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "富士重工業"}], "nameIdentifiers": [{"nameIdentifier": "425006", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "National Aerospace Laboratory", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "425007", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Mitsubishi Heavy Industries Ltd", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "425008", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kawasaki Heavy Industries Ltd", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "425009", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Fuji Heavy Industries Ltd", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "425010", "nameIdentifierScheme": "WEKO"}]}]}, "item_files": {"attribute_name": "ファイル情報", "attribute_type": "file", "attribute_value_mlt": [{"accessrole": "open_date", "date": [{"dateType": "Available", "dateValue": "2020-01-24"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "nalsp00031.pdf", "filesize": [{"value": "18.6 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 18600000.0, "url": {"label": "nalsp00031.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/36823/files/nalsp00031.pdf"}, "version_id": "3324251b-fa08-4aec-947b-af57f4da9d72"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "革新航空機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "要素技術", "subitem_subject_scheme": "Other"}, {"subitem_subject": "航空機モデル", "subitem_subject_scheme": "Other"}, {"subitem_subject": "オイル流れの可視化", "subitem_subject_scheme": "Other"}, {"subitem_subject": "抗力測定", "subitem_subject_scheme": "Other"}, {"subitem_subject": "境界層遷移", "subitem_subject_scheme": "Other"}, {"subitem_subject": "圧縮性境界層", "subitem_subject_scheme": "Other"}, {"subitem_subject": "線形安定性解析", "subitem_subject_scheme": "Other"}, {"subitem_subject": "遷移予測", "subitem_subject_scheme": "Other"}, {"subitem_subject": "圧縮性層流制御", "subitem_subject_scheme": "Other"}, {"subitem_subject": "熱伝導コード", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ファスナー接合要素解析", "subitem_subject_scheme": "Other"}, {"subitem_subject": "熱伝導", "subitem_subject_scheme": "Other"}, {"subitem_subject": "熱伝達", "subitem_subject_scheme": "Other"}, {"subitem_subject": "軽金属材料", "subitem_subject_scheme": "Other"}, {"subitem_subject": "advanced aircraft", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "component technology", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aircraft model", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "oil flow visualization", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "drag measurement", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "boundary layer transition", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "compressible boundary layer", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "linear stability analysis", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "transition estimation", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "compressible laminar flow control", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "heat conduction code", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "fastener jointed component analysis", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "heat conduction", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "thermal transfer", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "light metallic material", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}]}, "item_language": {"attribute_name": "言語", "attribute_value_mlt": [{"subitem_language": "eng"}]}, "item_resource_type": {"attribute_name": "資源タイプ", "attribute_value_mlt": [{"resourcetype": "conference paper", "resourceuri": "http://purl.org/coar/resource_type/c_5794"}]}, "item_title": "Government-industry specific joint research on the advanced aircraft component technologies, Final report", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "Government-industry specific joint research on the advanced aircraft component technologies, Final report", "subitem_title_language": "en"}]}, "item_type_id": "5", "owner": "1", "path": ["1891", "1915"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/36823", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "36823", "relation": {}, "relation_version_is_last": true, "title": ["Government-industry specific joint research on the advanced aircraft component technologies, Final report"], "weko_shared_id": 1}
Government-industry specific joint research on the advanced aircraft component technologies, Final report
https://jaxa.repo.nii.ac.jp/records/36823
https://jaxa.repo.nii.ac.jp/records/368233d498ff1-2cb1-46c6-8a3c-fa4f7edd2cad
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp00031.pdf (18.6 MB)
|
|
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Government-industry specific joint research on the advanced aircraft component technologies, Final report | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 革新航空機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 要素技術 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空機モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | オイル流れの可視化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 抗力測定 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層遷移 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧縮性境界層 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 線形安定性解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷移予測 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧縮性層流制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱伝導コード | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ファスナー接合要素解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱伝導 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱伝達 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軽金属材料 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | advanced aircraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | component technology | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aircraft model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | oil flow visualization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | drag measurement | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer transition | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | compressible boundary layer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | linear stability analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transition estimation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | compressible laminar flow control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat conduction code | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | fastener jointed component analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat conduction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal transfer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | light metallic material | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル | ||||||
その他のタイトル | 革新航空機要素技術についての政府産業界特別共同研究 | |||||
著者 |
航空宇宙技術研究所
× 航空宇宙技術研究所× 三菱重工業× 川崎重工業× 富士重工業× National Aerospace Laboratory× Mitsubishi Heavy Industries Ltd× Kawasaki Heavy Industries Ltd× Fuji Heavy Industries Ltd |
|||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
川崎重工業 | ||||||
著者所属 | ||||||
富士重工業 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries, Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries, Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Heavy Industries, Ltd | ||||||
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特別資料 en : Special Publication of National Aerospace Laboratory 巻 31, p. 1-168, 発行日 1996-05 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 以下の主題について論じた。オイル流れの可視化、抗力測定、3次元境界層遷移、圧縮性境界層、超音速層流制御、圧縮性層流制御、ファスナー接合要素解析、ファスナー接合構造要素における熱伝導、流体と構造物間の熱伝達、超音速機用軽金属材料、超音速機用繊維/金属ラミネート、耐損傷胴体構造解析、炭素繊維強化プラスチック複合部材の非破壊評価、T字型補強部材の座屈、および補強部材の表皮剥離。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The following topics were discussed: oil flow visualization, drag measurement, three dimensional boundary layer transition, compressible boundary layers, supersonic laminar flow control, compressible laminar flow control, fastener jointed component analysis, heat conduction in fastener jointed structural components, thermal transfer between fluid and structure, light metallic materials for supersonic transport, fiber/metal laminates for supersonic transport, damage tolerant fuselage structure analysis, nondestructive evaluation for carbon fiber reinforced plastic composites member, buckling of T-shaped stiffener, and skin disbond of stiffener. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0000440000 | |||||
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 SP-31 |