WEKO3
アイテム
{"_buckets": {"deposit": "023b1228-7347-42f1-b003-5d36f6b87341"}, "_deposit": {"created_by": 1, "id": "36911", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "36911"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00036911", "sets": ["1891", "1915"]}, "author_link": ["478180", "478179"], "item_5_alternative_title_1": {"attribute_name": "その他のタイトル", "attribute_value_mlt": [{"subitem_alternative_title": "翼を通過する亜音速流のシミュレーション"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1997-01", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "300", "bibliographicPageStart": "295", "bibliographicVolumeNumber": "34", "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_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 6-7 JUN. 1996 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 6-7 JUN. 1996 Tokyo Japan", "subitem_description_type": "Other"}]}, "item_5_description_16": {"attribute_name": "抄録", "attribute_value_mlt": [{"subitem_description": "ナビエ・ストークス方程式を解いて高レイノルズ非圧縮性流のシミュレーションを行った。乱流モデルを使わずに3次風上差分法を適用し、また多重方向のスキームも用いた。翼まわりの数値計算でで未解決問題に着手し、数値計算研究法の可能性を大幅に広げる新たな結果を紹介した。同じ研究法を用いて、負の厚さの翼の概念を導入し、この概念の適用を提案した。", "subitem_description_type": "Abstract"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "Incompressible high-Reynolds-number flow are simulated by solving the Navier-Stokes equations. A finite-difference method with third-order upwinding are employed without using any turbulence model. Also multi-directional method is used. Unsolved problems in computation around an airfoil are attacked and new results are presented, which will make the possibility of computational approach widen substantially. Using the same approach, a concept of an airfoil of negative thickness is introduced. Application of this concept is suggested.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0000685052", "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-34", "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": "宇宙科学研究所"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Astronautical Science"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "桑原, 邦郎"}], "nameIdentifiers": [{"nameIdentifier": "478179", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kuwahara, Kunio", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "478180", "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": "nalsp0034052.pdf", "filesize": [{"value": "1.1 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1100000.0, "url": {"label": "nalsp0034052.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/36911/files/nalsp0034052.pdf"}, "version_id": "5026a9ba-6036-451c-a5bd-9860d6a187d0"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "亜音速流", "subitem_subject_scheme": "Other"}, {"subitem_subject": "非圧縮性流", "subitem_subject_scheme": "Other"}, {"subitem_subject": "高レイノルズ流", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ナビエ・ストークス方程式", "subitem_subject_scheme": "Other"}, {"subitem_subject": "差分法", "subitem_subject_scheme": "Other"}, {"subitem_subject": "3次風上", "subitem_subject_scheme": "Other"}, {"subitem_subject": "乱流モデル", "subitem_subject_scheme": "Other"}, {"subitem_subject": "多重方向法", "subitem_subject_scheme": "Other"}, {"subitem_subject": "負の厚さ翼", "subitem_subject_scheme": "Other"}, {"subitem_subject": "subsonic flow", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "incompressible flow", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "high Reynolds number flow", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Navier Stokes equation", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "finite difference method", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "three order winding", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "turbulence model", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "multi directional method", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "negative thickness airfoil", "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": "Simulation of subsonic flow past an airfoil", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "Simulation of subsonic flow past an airfoil", "subitem_title_language": "en"}]}, "item_type_id": "5", "owner": "1", "path": ["1891", "1915"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/36911", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "36911", "relation": {}, "relation_version_is_last": true, "title": ["Simulation of subsonic flow past an airfoil"], "weko_shared_id": -1}
Simulation of subsonic flow past an airfoil
https://jaxa.repo.nii.ac.jp/records/36911
https://jaxa.repo.nii.ac.jp/records/369110e3104d7-448b-46a2-915d-646b2dad863e
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp0034052.pdf (1.1 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 | Simulation of subsonic flow past an airfoil | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 亜音速流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非圧縮性流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高レイノルズ流 | |||||
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 | 差分法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3次風上 | |||||
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 | 多重方向法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 負の厚さ翼 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | subsonic flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | incompressible flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high Reynolds number flow | |||||
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 | finite difference method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three order winding | |||||
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 | multi directional method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | negative thickness airfoil | |||||
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 | 翼を通過する亜音速流のシミュレーション | |||||
著者 |
桑原, 邦郎
× 桑原, 邦郎× Kuwahara, Kunio |
|||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science | ||||||
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 34, p. 295-300, 発行日 1997-01 |
|||||
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 6-7 JUN. 1996 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 6-7 JUN. 1996 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | ナビエ・ストークス方程式を解いて高レイノルズ非圧縮性流のシミュレーションを行った。乱流モデルを使わずに3次風上差分法を適用し、また多重方向のスキームも用いた。翼まわりの数値計算でで未解決問題に着手し、数値計算研究法の可能性を大幅に広げる新たな結果を紹介した。同じ研究法を用いて、負の厚さの翼の概念を導入し、この概念の適用を提案した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Incompressible high-Reynolds-number flow are simulated by solving the Navier-Stokes equations. A finite-difference method with third-order upwinding are employed without using any turbulence model. Also multi-directional method is used. Unsolved problems in computation around an airfoil are attacked and new results are presented, which will make the possibility of computational approach widen substantially. Using the same approach, a concept of an airfoil of negative thickness is introduced. Application of this concept is suggested. | |||||
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: AA0000685052 | |||||
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-34 |