WEKO3
アイテム
{"_buckets": {"deposit": "54086ea7-16fa-4273-931f-2df1959fef95"}, "_deposit": {"created_by": 1, "id": "37727", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "37727"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00037727", "sets": ["1891", "1915"]}, "author_link": ["482696", "482693", "482692", "482695", "482697", "482694"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Numerical analysis of laminar flow in S-curved square duct with inlet and outlet straight region"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1992-12", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "228", "bibliographicPageStart": "225", "bibliographicVolumeNumber": "19", "bibliographic_titles": [{"bibliographic_title": "航空宇宙技術研究所特別資料: 第10回航空機計算空気力学シンポジウム論文集"}, {"bibliographic_title": "Special Publication of National Aerospace Laboratory: Proceedings of the NAL symposium on aircraft computational aerodynamics", "bibliographic_titleLang": "en"}]}]}, "item_5_description_14": {"attribute_name": "会議概要(会議名, 開催地, 会期, 主催者等)", "attribute_value_mlt": [{"subitem_description": "航空宇宙技術研究所 10-12 Jun. 1992 東京 日本", "subitem_description_type": "Other"}]}, "item_5_description_15": {"attribute_name": "会議概要(会議名, 開催地, 会期, 主催者等)(英)", "attribute_value_mlt": [{"subitem_description": "National Aerospace Laboratory 10-12 Jun. 1992 Tokyo Japan", "subitem_description_type": "Other"}]}, "item_5_description_16": {"attribute_name": "抄録", "attribute_value_mlt": [{"subitem_description": "真直ぐな入口および出口部分をもつ正方形断面S字ダクトの中の発達する層流を有限容積法に基づいて数値的に調べた。ディーン数は299、曲率比は7で、S字ダクト角は22.5度である。計算結果をTaylorらによる実験データと比較し、良好な一致をみた。", "subitem_description_type": "Abstract"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "Developing laminar flow in a S-curved square duct with an inlet and outlet straight region, is studied numerically by using a finite volume method. In this study, Dean number is 299 and curvature ratio is 7 and S-curved duct angle is 22.5 degrees respectively. Calculated results are compared with the experimental data by Taylor et al.. The calculated results showed good agreements with the experimental data.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0004168041", "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-19", "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 角田支所"}, {"subitem_text_value": "航空宇宙技術研究所 角田支所"}, {"subitem_text_value": "航空宇宙技術研究所 角田支所"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "National Aerospace Laboratory Kakuda Research Center"}, {"subitem_text_language": "en", "subitem_text_value": "National Aerospace Laboratory Kakuda Research Center"}, {"subitem_text_language": "en", "subitem_text_value": "National Aerospace Laboratory Kakuda Research Center"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "山田, 仁"}], "nameIdentifiers": [{"nameIdentifier": "482692", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "石垣, 博"}], "nameIdentifiers": [{"nameIdentifier": "482693", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "望月, 宗和"}], "nameIdentifiers": [{"nameIdentifier": "482694", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Yamada, Hitoshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "482695", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ishigaki, Hiroshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "482696", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Mochizuki, Munekazu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "482697", "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": "2020-02-10"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "nalsp0019041.pdf", "filesize": [{"value": "259.5 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 259500.0, "url": {"label": "nalsp0019041.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/37727/files/nalsp0019041.pdf"}, "version_id": "0b8103d9-8165-405e-a857-2a6bb852b120"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "S字ダクト流れ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "曲り管内流れ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ダクト内層流", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ダクト曲率効果", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ダクト壁面摩擦", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ダクト内速度プロフィール", "subitem_subject_scheme": "Other"}, {"subitem_subject": "流れ数値シミュレーション", "subitem_subject_scheme": "Other"}, {"subitem_subject": "流れ数値解析", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD解析", "subitem_subject_scheme": "Other"}, {"subitem_subject": "計算流体力学解析", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ナビエ・ストークス方程式", "subitem_subject_scheme": "Other"}, {"subitem_subject": "内部流", "subitem_subject_scheme": "Other"}, {"subitem_subject": "パイプ内流れ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "S shape duct flow", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "curved duct flow", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "laminar duct flow", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "duct curvature effect", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "duct wall friction", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "duct velocity profile", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "numerical flow simulation", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "numerical flow analysis", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD analysis", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "computational fluid dynamics analysis", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Navier Stokes equation", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "internal flow", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "pipe flow", "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": "S型ベンドの流れの数値解析", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "S型ベンドの流れの数値解析"}]}, "item_type_id": "5", "owner": "1", "path": ["1891", "1915"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/37727", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "37727", "relation": {}, "relation_version_is_last": true, "title": ["S型ベンドの流れの数値解析"], "weko_shared_id": -1}
S型ベンドの流れの数値解析
https://jaxa.repo.nii.ac.jp/records/37727
https://jaxa.repo.nii.ac.jp/records/37727d889dbef-eccb-46ba-8546-2792792dd251
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp0019041.pdf (259.5 kB)
|
|
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 | S型ベンドの流れの数値解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | S字ダクト流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 曲り管内流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ダクト内層流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ダクト曲率効果 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ダクト壁面摩擦 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ダクト内速度プロフィール | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ数値解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算流体力学解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ナビエ・ストークス方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 内部流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | パイプ内流れ | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | S shape duct flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | curved duct flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laminar duct flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | duct curvature effect | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | duct wall friction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | duct velocity profile | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical flow simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical flow analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Navier Stokes equation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | internal flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pipe flow | |||||
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 | Numerical analysis of laminar flow in S-curved square duct with inlet and outlet straight region | |||||
著者 |
山田, 仁
× 山田, 仁× 石垣, 博× 望月, 宗和× Yamada, Hitoshi× Ishigaki, Hiroshi× Mochizuki, Munekazu |
|||||
著者所属 | ||||||
航空宇宙技術研究所 角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 角田支所 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Kakuda Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Kakuda Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Kakuda Research Center | ||||||
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: 第10回航空機計算空気力学シンポジウム論文集 en : Special Publication of National Aerospace Laboratory: Proceedings of the NAL symposium on aircraft computational aerodynamics 巻 19, p. 225-228, 発行日 1992-12 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 航空宇宙技術研究所 10-12 Jun. 1992 東京 日本 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | National Aerospace Laboratory 10-12 Jun. 1992 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 真直ぐな入口および出口部分をもつ正方形断面S字ダクトの中の発達する層流を有限容積法に基づいて数値的に調べた。ディーン数は299、曲率比は7で、S字ダクト角は22.5度である。計算結果をTaylorらによる実験データと比較し、良好な一致をみた。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Developing laminar flow in a S-curved square duct with an inlet and outlet straight region, is studied numerically by using a finite volume method. In this study, Dean number is 299 and curvature ratio is 7 and S-curved duct angle is 22.5 degrees respectively. Calculated results are compared with the experimental data by Taylor et al.. The calculated results showed good agreements with the experimental data. | |||||
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: AA0004168041 | |||||
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-19 |