WEKO3
アイテム
{"_buckets": {"deposit": "879b8c30-6a9b-4fd9-909e-e8fa0cea477c"}, "_deposit": {"created_by": 1, "id": "6454", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "6454"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00006454", "sets": ["1073", "1891"]}, "author_link": ["32804", "32805", "32806", "32803"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "CFD analysis and validation study of the 2-D high lift devices"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2005-03-25", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "92", "bibliographicPageStart": "87", "bibliographicVolumeNumber": "JAXA-SP-04-012", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2004論文集"}, {"bibliographic_title": "JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004", "bibliographic_titleLang": "en"}]}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "This paper presents numerical study on the 2-D high lift devices (HLD). CFD analyses of 2 element (NLR-7301) and 4 element (Boeing Model C) airfoils was conducted, using 2 different CFD codes (JAXA UPACS and MHI in-house codes). MHI in-house code adopts overset grid method. A new method of overset pattern optimization was developed, and grid dependency due to interpolation process is reduced by this method. The detail process of the method is described. Through the validation study, both CFD results agree well with WTT results. However, through the careful investigation of the CFD results, it was found that turbulence transition treatment of CFD highly affected the estimation of HLD aerodynamic characteristics. Finally, it comes to the conclusion that accurate prediction of the transition location is necessary for that of aerodynamic characteristics of HLD.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0048469014", "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-04-012", "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": "数値解析"}, {"subitem_text_value": "航空力学"}, {"subitem_text_value": "航空機の設計、試験及び性能"}]}, "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_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_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": "三菱重工業"}, {"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Mitsubishi Heavy Industries Ltd."}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "竹中, 啓三"}], "nameIdentifiers": [{"nameIdentifier": "32803", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "山本, 一臣"}], "nameIdentifiers": [{"nameIdentifier": "32804", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Takenaka, Keizo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "32805", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Yamamoto, Kazuomi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "32806", "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": "48469014.pdf", "filesize": [{"value": "1.9 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1900000.0, "url": {"label": "48469014.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/6454/files/48469014.pdf"}, "version_id": "027b9043-27eb-48d0-ab39-1c2c2bd278ad"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "2次元物体", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD", "subitem_subject_scheme": "Other"}, {"subitem_subject": "流れ場解析", "subitem_subject_scheme": "Other"}, {"subitem_subject": "高揚力装置", "subitem_subject_scheme": "Other"}, {"subitem_subject": "計算格子", "subitem_subject_scheme": "Other"}, {"subitem_subject": "格子依存性", "subitem_subject_scheme": "Other"}, {"subitem_subject": "パターン最適化", "subitem_subject_scheme": "Other"}, {"subitem_subject": "空力特性", "subitem_subject_scheme": "Other"}, {"subitem_subject": "実証", "subitem_subject_scheme": "Other"}, {"subitem_subject": "航空機設計", "subitem_subject_scheme": "Other"}, {"subitem_subject": "two dimensional body", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flow analysis", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "high lift device", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "computational grid", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "grid dependency", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "pattern optimization", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aerodynamic characteristic", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "validation", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aircraft design", "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": "2次元高揚力装置周りの流れ場解析とその検証", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "2次元高揚力装置周りの流れ場解析とその検証"}]}, "item_type_id": "5", "owner": "1", "path": ["1073", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/6454", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "6454", "relation": {}, "relation_version_is_last": true, "title": ["2次元高揚力装置周りの流れ場解析とその検証"], "weko_shared_id": -1}
2次元高揚力装置周りの流れ場解析とその検証
https://jaxa.repo.nii.ac.jp/records/6454
https://jaxa.repo.nii.ac.jp/records/645490f8eb74-6442-4c30-be83-d23cbadc7c70
名前 / ファイル | ライセンス | アクション |
---|---|---|
48469014.pdf (1.9 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 | 2次元高揚力装置周りの流れ場解析とその検証 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2次元物体 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ場解析 | |||||
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 | 計算格子 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 格子依存性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | パターン最適化 | |||||
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 | 実証 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空機設計 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two dimensional body | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow analysis | |||||
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 | computational grid | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | grid dependency | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pattern optimization | |||||
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 | validation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aircraft design | |||||
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 and validation study of the 2-D high lift devices | |||||
著者 |
竹中, 啓三
× 竹中, 啓三× 山本, 一臣× Takenaka, Keizo× Yamamoto, Kazuomi |
|||||
著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
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: 航空宇宙数値シミュレーション技術シンポジウム2004論文集 en : JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004 巻 JAXA-SP-04-012, p. 87-92, 発行日 2005-03-25 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents numerical study on the 2-D high lift devices (HLD). CFD analyses of 2 element (NLR-7301) and 4 element (Boeing Model C) airfoils was conducted, using 2 different CFD codes (JAXA UPACS and MHI in-house codes). MHI in-house code adopts overset grid method. A new method of overset pattern optimization was developed, and grid dependency due to interpolation process is reduced by this method. The detail process of the method is described. Through the validation study, both CFD results agree well with WTT results. However, through the careful investigation of the CFD results, it was found that turbulence transition treatment of CFD highly affected the estimation of HLD aerodynamic characteristics. Finally, it comes to the conclusion that accurate prediction of the transition location is necessary for that of aerodynamic characteristics of HLD. | |||||
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: AA0048469014 | |||||
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-04-012 |