WEKO3
アイテム
{"_buckets": {"deposit": "390cd87a-7e60-43e5-860d-9a0ba215569d"}, "_deposit": {"created_by": 1, "id": "43181", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "43181"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00043181", "sets": ["1893", "1915"]}, "author_link": ["462519", "462521", "462520", "462518"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Numerical Simulation of an Aircraft Icing"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1985-11", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "6", "bibliographicPageStart": "1", "bibliographicVolumeNumber": "5", "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 SP-5", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "A finite difference method was developed to simulate aircraft icing. An air flow was calculated by solving compressible Navier-Stokes equations directly. The accretion of ice to the NACA0012 airfoil at various angles of attack was calculated from trajectries of supercooled liquid drops through that flow.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: NALSP0005001", "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 SP-5", "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": "0289-260X", "subitem_source_identifier_type": "ISSN"}]}, "item_3_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_3_text_34": {"attribute_name": "メタデータ提供者", "attribute_value_mlt": [{"subitem_text_value": "メタデータ提供者: NAL-MATCH"}]}, "item_3_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_3_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: AP"}]}, "item_3_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: 9"}]}, "item_3_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "東京大学"}, {"subitem_text_value": "宇宙科学研究所"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "高橋, 大輔"}], "nameIdentifiers": [{"nameIdentifier": "462518", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "桑原, 邦郎"}], "nameIdentifiers": [{"nameIdentifier": "462519", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Takahashi, Daisuke", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "462520", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kuwahara, Kunio", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "462521", "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": "2020-01-28"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "nalsp0005001.pdf", "filesize": [{"value": "406.4 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 406400.0, "url": {"label": "nalsp0005001.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/43181/files/nalsp0005001.pdf"}, "version_id": "ea25a914-ea87-4d81-b58d-54dec16b1acd"}]}, "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": "アイシングのシミュレーション", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "アイシングのシミュレーション"}]}, "item_type_id": "3", "owner": "1", "path": ["1893", "1915"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/43181", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "43181", "relation": {}, "relation_version_is_last": true, "title": ["アイシングのシミュレーション"], "weko_shared_id": -1}
アイシングのシミュレーション
https://jaxa.repo.nii.ac.jp/records/43181
https://jaxa.repo.nii.ac.jp/records/431814b424f82-c07a-4a75-b01b-0d39be51d20c
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp0005001.pdf (406.4 kB)
|
|
Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | アイシングのシミュレーション | |||||
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 | Numerical Simulation of an Aircraft Icing | |||||
著者 |
高橋, 大輔
× 高橋, 大輔× 桑原, 邦郎× Takahashi, Daisuke× Kuwahara, Kunio |
|||||
著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
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 SP-5 巻 5, p. 1-6, 発行日 1985-11 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A finite difference method was developed to simulate aircraft icing. An air flow was calculated by solving compressible Navier-Stokes equations directly. The accretion of ice to the NACA0012 airfoil at various angles of attack was calculated from trajectries of supercooled liquid drops through that flow. | |||||
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: NALSP0005001 | |||||
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-5 |