WEKO3
アイテム
{"_buckets": {"deposit": "3cdb072c-03f2-44c8-ad75-03513e529f9e"}, "_deposit": {"created_by": 1, "id": "14676", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "14676"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00014676", "sets": ["1669", "1891"]}, "author_link": ["134076", "134078", "134081", "134079", "134080", "134082", "134083", "134077"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Study on flowfield around winged TSTO launch vehicle by visualization using the electrical discharge method"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2004-05", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "122", "bibliographicPageStart": "119", "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": "The visualization of flowfield around a winged TSTO (Two Stage To Orbit) launch vehicle model has been carried out using the electrical discharge method. In this report, boundary layers and three-dimensional (lateral and cross-sectional) shock shapes around the model are demonstrated. The existence of a separation shock is confirmed three-dimensionally. The experiments are carried out using a hypersonic gun tunnel, with Mach number of 10 and duration of 10 ms.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0047120031", "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": "計装(計測制御装置の装備技術)及び写真技術"}, {"subitem_text_value": "航空力学"}, {"subitem_text_value": "宇宙船設計、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: 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": "福山大学 大学院"}, {"subitem_text_value": "福山大学 大学院"}, {"subitem_text_value": "福山大学 工学部"}, {"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": "Fukuyama University Graduate School"}, {"subitem_text_language": "en", "subitem_text_value": "Fukuyama University Graduate School"}, {"subitem_text_language": "en", "subitem_text_value": "Fukuyama University Faculty of Engineering"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}]}, "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": "瀬崎, 新士"}], "nameIdentifiers": [{"nameIdentifier": "134076", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "中村, 弘明"}], "nameIdentifiers": [{"nameIdentifier": "134077", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "西尾, 正富"}], "nameIdentifiers": [{"nameIdentifier": "134078", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "山本, 行光"}], "nameIdentifiers": [{"nameIdentifier": "134079", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Sezaki, Shinji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "134080", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nakamura, Hiroaki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "134081", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nishio, Masatomi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "134082", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Yamamoto, Yukimitsu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "134083", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "再使用型宇宙機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "TSTO", "subitem_subject_scheme": "Other"}, {"subitem_subject": "再使用型打上げ機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "衝撃波-境界層干渉", "subitem_subject_scheme": "Other"}, {"subitem_subject": "極超音速飛行", "subitem_subject_scheme": "Other"}, {"subitem_subject": "流れの可視化", "subitem_subject_scheme": "Other"}, {"subitem_subject": "風洞試験", "subitem_subject_scheme": "Other"}, {"subitem_subject": "境界層剥離", "subitem_subject_scheme": "Other"}, {"subitem_subject": "放電", "subitem_subject_scheme": "Other"}, {"subitem_subject": "reusable spacecraft", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "TSTO", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "reusable launch vehicle", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "shock wave-boundary layer interaction", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "hypersonic flight", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flow visualization", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "wind tunnel test", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "boundary layer separation", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "electric discharge", "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": "有翼TSTO宇宙往還機周りの流れ場の放電発光法による可視化研究", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "有翼TSTO宇宙往還機周りの流れ場の放電発光法による可視化研究"}]}, "item_type_id": "5", "owner": "1", "path": ["1669", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/14676", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "14676", "relation": {}, "relation_version_is_last": true, "title": ["有翼TSTO宇宙往還機周りの流れ場の放電発光法による可視化研究"], "weko_shared_id": -1}
有翼TSTO宇宙往還機周りの流れ場の放電発光法による可視化研究
https://jaxa.repo.nii.ac.jp/records/14676
https://jaxa.repo.nii.ac.jp/records/146762cb24bbd-74d9-4ee4-b199-ed4b4dadda70
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 | 有翼TSTO宇宙往還機周りの流れ場の放電発光法による可視化研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再使用型宇宙機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | TSTO | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再使用型打上げ機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝撃波-境界層干渉 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速飛行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れの可視化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層剥離 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 放電 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reusable spacecraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | TSTO | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reusable launch vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shock wave-boundary layer interaction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic flight | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow visualization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer separation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | electric discharge | |||||
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 | Study on flowfield around winged TSTO launch vehicle by visualization using the electrical discharge method | |||||
著者 |
瀬崎, 新士
× 瀬崎, 新士× 中村, 弘明× 西尾, 正富× 山本, 行光× Sezaki, Shinji× Nakamura, Hiroaki× Nishio, Masatomi× Yamamoto, Yukimitsu |
|||||
著者所属 | ||||||
福山大学 大学院 | ||||||
著者所属 | ||||||
福山大学 大学院 | ||||||
著者所属 | ||||||
福山大学 工学部 | ||||||
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 | ||||||
Fukuyama University Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
Fukuyama University Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
Fukuyama University Faculty of Engineering | ||||||
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. 119-122, 発行日 2004-05 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The visualization of flowfield around a winged TSTO (Two Stage To Orbit) launch vehicle model has been carried out using the electrical discharge method. In this report, boundary layers and three-dimensional (lateral and cross-sectional) shock shapes around the model are demonstrated. The existence of a separation shock is confirmed three-dimensionally. The experiments are carried out using a hypersonic gun tunnel, with Mach number of 10 and duration of 10 ms. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047120031 |