WEKO3
アイテム
{"_buckets": {"deposit": "b3f34314-0709-4150-8b97-06959effd020"}, "_deposit": {"created_by": 1, "id": "14662", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "14662"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00014662", "sets": ["1669", "1891"]}, "author_link": ["133963", "133964", "133965", "133962"], "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 an aerodynamic body-flap effect for a basic SSTO-rocket configuration"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2004-05", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "66", "bibliographicPageStart": "63", "bibliographic_titles": [{"bibliographic_title": "宇宙航行の力学シンポジウム 平成15年度"}, {"bibliographic_title": "Symposium on Flight Mechanics and Astrodynamics 2003", "bibliographic_titleLang": "en"}]}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "Navier-Stokes simulations are carried out for the investigation of a body-flap effect on the subsonic to supersonic base-entry aerodynamic characteristics for the conical SSTO-rocket configuration. It is clarified that the body-flap effect has strong dependence on the angle of attack and Mach number. The body-flap effect is small at subsonic and transonic conditions. At the subsonic and transonic conditions, the windside pressure level over the body-flap is not so high as compared to the leeside due to the influence of the flow which is accelerated over the base surface. It is also clarified that the pressure level behind the body-flap does not become lower than that in the recirculating flow behind the body in all the subsonic to supersonic conditions.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0047120017", "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宇宙科学研究本部"}]}, "item_5_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)"}]}, "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": "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: シンポジウム・研究会"}]}, "item_5_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: IS"}]}, "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: 010"}]}, "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": "東京大学 大学院"}, {"subitem_text_value": "宇宙航空研究開発機構 宇宙科学研究本部"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "University of Tokyo Graduate School"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]}, "item_access_right": {"attribute_name": "アクセス権", "attribute_value_mlt": [{"subitem_access_right": "metadata only access", "subitem_access_right_uri": "http://purl.org/coar/access_right/c_14cb"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "藤本, 圭一郎"}], "nameIdentifiers": [{"nameIdentifier": "133962", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "藤井, 孝蔵"}], "nameIdentifiers": [{"nameIdentifier": "133963", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Fujimoto, Keiichiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "133964", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Fujii, Kozo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "133965", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "再使用型ロケット", "subitem_subject_scheme": "Other"}, {"subitem_subject": "SSTOロケット", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ボディフラップ効果", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD", "subitem_subject_scheme": "Other"}, {"subitem_subject": "迎角", "subitem_subject_scheme": "Other"}, {"subitem_subject": "マッハ数", "subitem_subject_scheme": "Other"}, {"subitem_subject": "空力特性", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Baldwin-Lomax乱流モデル", "subitem_subject_scheme": "Other"}, {"subitem_subject": "reusable rocket", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "SSTO-rocket", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "body-flap effect", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "angle of attack", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Mach number", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aerodynamic characteristic", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Baldwin-Lomax turbulence model", "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": "単段再使用ロケットにおけるボディフラップ効果のCFD解析", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "単段再使用ロケットにおけるボディフラップ効果のCFD解析"}]}, "item_type_id": "5", "owner": "1", "path": ["1669", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/14662", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "14662", "relation": {}, "relation_version_is_last": true, "title": ["単段再使用ロケットにおけるボディフラップ効果のCFD解析"], "weko_shared_id": -1}
単段再使用ロケットにおけるボディフラップ効果のCFD解析
https://jaxa.repo.nii.ac.jp/records/14662
https://jaxa.repo.nii.ac.jp/records/146628ca3717e-d691-4f95-8f4f-6575ef2eeadd
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 | 単段再使用ロケットにおけるボディフラップ効果のCFD解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再使用型ロケット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | SSTOロケット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ボディフラップ効果 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 迎角 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | マッハ数 | |||||
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 | Baldwin-Lomax乱流モデル | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reusable rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SSTO-rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | body-flap effect | |||||
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 | angle of attack | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mach number | |||||
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 | Baldwin-Lomax turbulence model | |||||
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 | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | CFD analysis of an aerodynamic body-flap effect for a basic SSTO-rocket configuration | |||||
著者 |
藤本, 圭一郎
× 藤本, 圭一郎× 藤井, 孝蔵× Fujimoto, Keiichiro× Fujii, Kozo |
|||||
著者所属 | ||||||
東京大学 大学院 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
宇宙航行の力学シンポジウム 平成15年度 en : Symposium on Flight Mechanics and Astrodynamics 2003 p. 63-66, 発行日 2004-05 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Navier-Stokes simulations are carried out for the investigation of a body-flap effect on the subsonic to supersonic base-entry aerodynamic characteristics for the conical SSTO-rocket configuration. It is clarified that the body-flap effect has strong dependence on the angle of attack and Mach number. The body-flap effect is small at subsonic and transonic conditions. At the subsonic and transonic conditions, the windside pressure level over the body-flap is not so high as compared to the leeside due to the influence of the flow which is accelerated over the base surface. It is also clarified that the pressure level behind the body-flap does not become lower than that in the recirculating flow behind the body in all the subsonic to supersonic conditions. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047120017 |