WEKO3
アイテム
{"_buckets": {"deposit": "5be1f5f3-cf6b-4535-a0eb-a6c93bc45b01"}, "_deposit": {"created_by": 1, "id": "5637", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "5637"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00005637", "sets": ["985", "1542", "1886", "1891"]}, "author_link": ["27649", "27651", "27648", "27653", "27650", "27652"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "CFD analysis of JAXA high-lift configuration model using overset mesh"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2008-02-29", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "195", "bibliographicPageStart": "190", "bibliographicVolumeNumber": "JAXA-SP-07-016", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料: 第39回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2007論文集"}, {"bibliographic_title": "JAXA Special Publication: Proceedings of 39th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2007", "bibliographic_titleLang": "en"}]}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "Flow around JAXA HLD (High Lift Devices) wind tunnel model is analyzed by RANS (Reynolds Averaged Navier Stokes) CFD (Computational Fluid Dynamics) method and compared with the experimental data obtained by JAXA. Unstructured mesh with overset technique is used for mesh generation around realistic configuration with small parts such as slat clip. It was shown that the slat clip made a difference in the flowfield especially around the edge of the slat. Baldwin-Barth and Spalart-Allmaras one equation models are used for turbulence model and the former gives better agreement with the experiment.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0063742031", "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: JAXA-SP-07-016", "subitem_description_type": "Other"}]}, "item_5_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "宇宙航空研究開発機構"}]}, "item_5_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Japan Aerospace Exploration Agency (JAXA)"}]}, "item_5_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "1349-113X", "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": "AA11984031", "subitem_source_identifier_type": "NCID"}]}, "item_5_text_20": {"attribute_name": "その他キーワード", "attribute_value_mlt": [{"subitem_text_value": "航空力学"}, {"subitem_text_value": "航空機の設計、試験及び性能"}, {"subitem_text_value": "数値解析"}]}, "item_5_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 特別資料"}]}, "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_40": {"attribute_name": "jaxa出版物種類", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物種類: SP"}]}, "item_5_text_41": {"attribute_name": "jaxa出版物シリーズ", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物シリーズ: 015"}]}, "item_5_text_42": {"attribute_name": "シンポジウム区分", "attribute_value_mlt": [{"subitem_text_value": "シンポジウム区分: 521"}]}, "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": "川崎重工業"}, {"subitem_text_value": "川崎重工業"}, {"subitem_text_value": "宇宙航空研究開発機構"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Kawasaki Heavy Industries Ltd."}, {"subitem_text_language": "en", "subitem_text_value": "Kawasaki Heavy Industries Ltd."}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "永田, 卓"}], "nameIdentifiers": [{"nameIdentifier": "27648", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "越智, 章生"}], "nameIdentifiers": [{"nameIdentifier": "27649", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "嶋, 英志"}], "nameIdentifiers": [{"nameIdentifier": "27650", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nagata, Taku", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "27651", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ochi, Akio", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "27652", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Shima, Eiji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "27653", "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": "2020-01-16"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "63742031.pdf", "filesize": [{"value": "1.6 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1600000.0, "url": {"label": "63742031.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/5637/files/63742031.pdf"}, "version_id": "4cae37ef-0538-40af-bab4-0f102bda0938"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "計算流体力学", "subitem_subject_scheme": "Other"}, {"subitem_subject": "風洞模型", "subitem_subject_scheme": "Other"}, {"subitem_subject": "高揚力装置", "subitem_subject_scheme": "Other"}, {"subitem_subject": "風洞試験", "subitem_subject_scheme": "Other"}, {"subitem_subject": "航空機設計", "subitem_subject_scheme": "Other"}, {"subitem_subject": "重合格子", "subitem_subject_scheme": "Other"}, {"subitem_subject": "格子生成", "subitem_subject_scheme": "Other"}, {"subitem_subject": "乱流モデル", "subitem_subject_scheme": "Other"}, {"subitem_subject": "流れの分布", "subitem_subject_scheme": "Other"}, {"subitem_subject": "空力抵抗", "subitem_subject_scheme": "Other"}, {"subitem_subject": "空力特性", "subitem_subject_scheme": "Other"}, {"subitem_subject": "レイノルズ平均化", "subitem_subject_scheme": "Other"}, {"subitem_subject": "前縁スラット", "subitem_subject_scheme": "Other"}, {"subitem_subject": "computational fluid dynamics", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "wind tunnel model", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "high-lift device", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "wind tunnel test", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aircraft design", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "overset mesh", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "grid generation", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "turbulence model", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flow distribution", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aerodynamic drag", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aerodynamic characteristic", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Reynolds averaging", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "leading edge slat", "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": "conference paper", "resourceuri": "http://purl.org/coar/resource_type/c_5794"}]}, "item_title": "重合格子を用いたJAXA高揚力装置風洞模型のCFD解析", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "重合格子を用いたJAXA高揚力装置風洞模型のCFD解析"}]}, "item_type_id": "5", "owner": "1", "path": ["985", "1542", "1886", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/5637", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "5637", "relation": {}, "relation_version_is_last": true, "title": ["重合格子を用いたJAXA高揚力装置風洞模型のCFD解析"], "weko_shared_id": -1}
重合格子を用いたJAXA高揚力装置風洞模型のCFD解析
https://jaxa.repo.nii.ac.jp/records/5637
https://jaxa.repo.nii.ac.jp/records/563731d16087-2030-408b-8ed9-fff8b5a8987d
名前 / ファイル | ライセンス | アクション |
---|---|---|
63742031.pdf (1.6 MB)
|
|
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 重合格子を用いたJAXA高揚力装置風洞模型のCFD解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞模型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高揚力装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空機設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 重合格子 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 格子生成 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 乱流モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れの分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力抵抗 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | レイノルズ平均化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 前縁スラット | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high-lift device | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aircraft design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | overset mesh | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | grid generation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbulence model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic drag | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Reynolds averaging | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | leading edge slat | |||||
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(英) | ||||||
その他のタイトル | CFD analysis of JAXA high-lift configuration model using overset mesh | |||||
著者 |
永田, 卓
× 永田, 卓× 越智, 章生× 嶋, 英志× Nagata, Taku× Ochi, Akio× Shima, Eiji |
|||||
著者所属 | ||||||
川崎重工業 | ||||||
著者所属 | ||||||
川崎重工業 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第39回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2007論文集 en : JAXA Special Publication: Proceedings of 39th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2007 巻 JAXA-SP-07-016, p. 190-195, 発行日 2008-02-29 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Flow around JAXA HLD (High Lift Devices) wind tunnel model is analyzed by RANS (Reynolds Averaged Navier Stokes) CFD (Computational Fluid Dynamics) method and compared with the experimental data obtained by JAXA. Unstructured mesh with overset technique is used for mesh generation around realistic configuration with small parts such as slat clip. It was shown that the slat clip made a difference in the flowfield especially around the edge of the slat. Baldwin-Barth and Spalart-Allmaras one equation models are used for turbulence model and the former gives better agreement with the experiment. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063742031 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-07-016 |