WEKO3
アイテム
{"_buckets": {"deposit": "ad82f1cb-7595-47fa-b111-a30df57ea3e7"}, "_deposit": {"created_by": 1, "id": "14658", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "14658"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00014658", "sets": ["1669", "1891"]}, "author_link": ["133931", "133933", "133935", "133932", "133930", "133929", "133934", "133928"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Study of flow structures around vehicle traveling at supersonic/hypersonic speeds"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2004-05", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "50", "bibliographicPageStart": "47", "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": "Flow structures around a hypersonic re-entry Mars Environmental Survey (MESUR) capsule traveling at supersonic/hypersonic speeds are investigated utilizing a new computational method based on the finite element method (FEM). In order to confirm the validity of the computational method the results are compared with experimental ones obtained by the electrical discharge method for hypersonic flow at Mach 10. From these results, it can be concluded that they were in good agreement. As an example of the numerical simulation, flowfields around the capsule traveling at a speed of Mach 5, 3, and 2, respectively, are investigated. By these simulations, differences of the flow structures for various Mach numbers are clarified. The result shows that the location of the separation behind the capsule is governed by the strength of the reverse pressure gradient. The reverse flow behind the capsule that determines the value of the base pressure distribution is correlated to the strength of the re-circulation region and the stability of the capsule.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0047120013", "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": "航空機の設計、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 工学部"}, {"subitem_text_value": "福山大学 大学院"}, {"subitem_text_value": "福山大学 工学部"}]}, "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 Faculty of Engineering"}, {"subitem_text_language": "en", "subitem_text_value": "Fukuyama University Graduate School"}, {"subitem_text_language": "en", "subitem_text_value": "Fukuyama University Faculty of Engineering"}]}, "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": "中村, 弘明"}], "nameIdentifiers": [{"nameIdentifier": "133928", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "真鍋, 圭司"}], "nameIdentifiers": [{"nameIdentifier": "133929", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "瀬崎, 新士"}], "nameIdentifiers": [{"nameIdentifier": "133930", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "西尾, 正富"}], "nameIdentifiers": [{"nameIdentifier": "133931", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nakamura, Hiroaki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "133932", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Manabe, Keiji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "133933", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Sezaki, Shinji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "133934", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nishio, Masatomi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "133935", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "流れの特性", "subitem_subject_scheme": "Other"}, {"subitem_subject": "超音速飛行", "subitem_subject_scheme": "Other"}, {"subitem_subject": "極超音速飛行", "subitem_subject_scheme": "Other"}, {"subitem_subject": "後流構造", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD", "subitem_subject_scheme": "Other"}, {"subitem_subject": "有限要素法", "subitem_subject_scheme": "Other"}, {"subitem_subject": "流れの可視化", "subitem_subject_scheme": "Other"}, {"subitem_subject": "レーザー誘起蛍光法", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flow characteristic", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "supersonic flight", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "hypersonic flight", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "wake structure", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "finite element method", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flow visualization", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "laser induced fluorescence", "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": "超音速/極超音速で飛行する飛翔体周りの流れ構造の研究", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "超音速/極超音速で飛行する飛翔体周りの流れ構造の研究"}]}, "item_type_id": "5", "owner": "1", "path": ["1669", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/14658", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "14658", "relation": {}, "relation_version_is_last": true, "title": ["超音速/極超音速で飛行する飛翔体周りの流れ構造の研究"], "weko_shared_id": -1}
超音速/極超音速で飛行する飛翔体周りの流れ構造の研究
https://jaxa.repo.nii.ac.jp/records/14658
https://jaxa.repo.nii.ac.jp/records/146587b2d0af5-98b2-43e5-b80a-c105fbcd843e
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 | 超音速/極超音速で飛行する飛翔体周りの流れ構造の研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れの特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速飛行 | |||||
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 | 後流構造 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 有限要素法 | |||||
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 | レーザー誘起蛍光法 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic flight | |||||
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 | wake structure | |||||
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 | finite element method | |||||
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 | laser induced fluorescence | |||||
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 of flow structures around vehicle traveling at supersonic/hypersonic speeds | |||||
著者 |
中村, 弘明
× 中村, 弘明× 真鍋, 圭司× 瀬崎, 新士× 西尾, 正富× Nakamura, Hiroaki× Manabe, Keiji× Sezaki, Shinji× Nishio, Masatomi |
|||||
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 | ||||||
福山大学 大学院 | ||||||
著者所属 | ||||||
福山大学 工学部 | ||||||
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 | ||||||
Fukuyama University Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
Fukuyama University Faculty of Engineering | ||||||
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. 47-50, 発行日 2004-05 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Flow structures around a hypersonic re-entry Mars Environmental Survey (MESUR) capsule traveling at supersonic/hypersonic speeds are investigated utilizing a new computational method based on the finite element method (FEM). In order to confirm the validity of the computational method the results are compared with experimental ones obtained by the electrical discharge method for hypersonic flow at Mach 10. From these results, it can be concluded that they were in good agreement. As an example of the numerical simulation, flowfields around the capsule traveling at a speed of Mach 5, 3, and 2, respectively, are investigated. By these simulations, differences of the flow structures for various Mach numbers are clarified. The result shows that the location of the separation behind the capsule is governed by the strength of the reverse pressure gradient. The reverse flow behind the capsule that determines the value of the base pressure distribution is correlated to the strength of the re-circulation region and the stability of the capsule. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047120013 |