WEKO3
アイテム
{"_buckets": {"deposit": "23e1c595-b12c-4e91-9706-7339ed638b36"}, "_deposit": {"created_by": 1, "id": "17369", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "17369"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00017369", "sets": ["1710", "1891"]}, "author_link": ["157624", "157623", "157620", "157625", "157622", "157621"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Development of accurate optimization method of the TSTO spaceplane: New aerodynamics model using CFD method"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2003-04", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "136", "bibliographicPageStart": "133", "bibliographic_titles": [{"bibliographic_title": "宇宙輸送シンポジウム 平成14年度"}, {"bibliographic_title": "Proceedings of Space Transportation Symposium FY2002", "bibliographic_titleLang": "en"}]}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "A new aerodynamics model is developed using the data obtained by accurate CFD simulations, as one of the components for the total optimization of TSTO systems. The developed component is integrated into the optimization program, and the influence of the new component is evaluated. Strong aerodynamic interaction occurs between the Booster and the Orbiter in the CFD simulations, and it indicates the importance of the accurate aerodynamics model. The optimization using the new aerodynamics model results in the heavier gross take-off weight compared to the result using the conventional aerodynamics model.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0045426033", "subitem_description_type": "Other"}]}, "item_5_text_20": {"attribute_name": "その他キーワード", "attribute_value_mlt": [{"subitem_text_value": "宇宙船設計、試験及び性能"}, {"subitem_text_value": "数値解析"}, {"subitem_text_value": "流体力学及び熱伝導"}]}, "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: 013"}]}, "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 大学院工学系研究科"}, {"subitem_text_value": "宇宙科学研究所"}, {"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": "University of Tokyo Graduate School of Engineering"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Astronautical Science"}, {"subitem_text_language": "en", "subitem_text_value": "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": "下山, 幸治"}], "nameIdentifiers": [{"nameIdentifier": "157620", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "藤井, 孝藏"}], "nameIdentifiers": [{"nameIdentifier": "157621", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "小林, 弘明"}], "nameIdentifiers": [{"nameIdentifier": "157622", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Shimoyama, Koji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "157623", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Fujii, Kozo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "157624", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kobayashi, Hiroaki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "157625", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "TSTOスペースプレーン", "subitem_subject_scheme": "Other"}, {"subitem_subject": "空力係数", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Baldwin-Lomax乱流モデル", "subitem_subject_scheme": "Other"}, {"subitem_subject": "軌道制御", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ブースターロケット", "subitem_subject_scheme": "Other"}, {"subitem_subject": "軌道機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "研究開発", "subitem_subject_scheme": "Other"}, {"subitem_subject": "TSTO spaceplane", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aerodynamic coefficient", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Baldwin-Lomax turbulence model", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "trajectory control", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "booster rocket", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "orbiter", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "research and development", "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": "TSTO統合最適設計の高度化:CFD解析によるTSTO空力評価モデルの構築", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "TSTO統合最適設計の高度化:CFD解析によるTSTO空力評価モデルの構築"}]}, "item_type_id": "5", "owner": "1", "path": ["1710", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/17369", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "17369", "relation": {}, "relation_version_is_last": true, "title": ["TSTO統合最適設計の高度化:CFD解析によるTSTO空力評価モデルの構築"], "weko_shared_id": -1}
TSTO統合最適設計の高度化:CFD解析によるTSTO空力評価モデルの構築
https://jaxa.repo.nii.ac.jp/records/17369
https://jaxa.repo.nii.ac.jp/records/17369d5c954da-beef-4ee8-8036-a45b2218e303
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 | TSTO統合最適設計の高度化:CFD解析によるTSTO空力評価モデルの構築 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | TSTOスペースプレーン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力係数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Baldwin-Lomax乱流モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ブースターロケット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 研究開発 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | TSTO spaceplane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic coefficient | |||||
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 | Baldwin-Lomax turbulence model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | trajectory control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | booster rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbiter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | research and development | |||||
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 | Development of accurate optimization method of the TSTO spaceplane: New aerodynamics model using CFD method | |||||
著者 |
下山, 幸治
× 下山, 幸治× 藤井, 孝藏× 小林, 弘明× Shimoyama, Koji× Fujii, Kozo× Kobayashi, Hiroaki |
|||||
著者所属 | ||||||
東京大学 大学院工学系研究科 | ||||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science | ||||||
書誌情報 |
宇宙輸送シンポジウム 平成14年度 en : Proceedings of Space Transportation Symposium FY2002 p. 133-136, 発行日 2003-04 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A new aerodynamics model is developed using the data obtained by accurate CFD simulations, as one of the components for the total optimization of TSTO systems. The developed component is integrated into the optimization program, and the influence of the new component is evaluated. Strong aerodynamic interaction occurs between the Booster and the Orbiter in the CFD simulations, and it indicates the importance of the accurate aerodynamics model. The optimization using the new aerodynamics model results in the heavier gross take-off weight compared to the result using the conventional aerodynamics model. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0045426033 |