{"created":"2023-06-20T13:42:47.575549+00:00","id":370,"links":{},"metadata":{"_buckets":{"deposit":"901320a6-0ba8-41b0-9b11-bf7b40e5f1c2"},"_deposit":{"created_by":2,"id":"370","owners":[2],"pid":{"revision_id":0,"type":"depid","value":"370"},"status":"published"},"_oai":{"id":"oai:fut.repo.nii.ac.jp:00000370","sets":["1"]},"author_link":["9741","9742","9744","9743"],"item_10002_biblio_info_7":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03-18","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"35","bibliographicPageEnd":"78","bibliographicPageStart":"71","bibliographic_titles":[{"bibliographic_title":"福井工業大学研究紀要. 第一部"}]}]},"item_10002_description_5":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"Optimum Mach number of hypersonic itransports has been setimated, where the energy cost becomes the lowest. The flight time and energy to reach a destination are obtained in cases of several flight types using several anagles of attack and ghrust powers. The model of a vehicle is a semi cone body with a triangle wing and its aerodynamic performances are calculated by considering the real gas effects. By considering the equivalent cost of consuming energy and flight, an potimum flight Mach number can be obtained.","subitem_description_type":"Abstract"}]},"item_10002_identifier_registration":{"attribute_name":"ID登録","attribute_value_mlt":[{"subitem_identifier_reg_text":"10.57375/00000364","subitem_identifier_reg_type":"JaLC"}]},"item_10002_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"福井工業大学"}]},"item_10002_relation_11":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_relation_type_id":{"subitem_relation_type_id_text":"TF00008823","subitem_relation_type_select":"NCID"}}]},"item_10002_source_id_9":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"2868571","subitem_source_identifier_type":"ISSN"}]},"item_10002_version_type_20":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"木村, 雄吉"}],"nameIdentifiers":[{"nameIdentifier":"9741","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"柳川, 聡寛"}],"nameIdentifiers":[{"nameIdentifier":"9742","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Kimura, Takeyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"9743","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Yanagawa, Toshihiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"9744","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":"2023-04-12"}],"displaytype":"detail","filename":"KJ00004179097.pdf","filesize":[{"value":"518.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"KJ00004179097.pdf","url":"https://fut.repo.nii.ac.jp/record/370/files/KJ00004179097.pdf"},"version_id":"bff280a1-6b3b-4db4-8c6a-698ba02c0a8c"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"極超音速旅客機における時間及びエネルギーに関する最適マッハ数予測","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"極超音速旅客機における時間及びエネルギーに関する最適マッハ数予測"},{"subitem_title":"Estimation of Optimum Mach Number due to Time and Energy for HST","subitem_title_language":"en"}]},"item_type_id":"10002","owner":"2","path":["1"],"pubdate":{"attribute_name":"公開日","attribute_value":"2009-04-04"},"publish_date":"2009-04-04","publish_status":"0","recid":"370","relation_version_is_last":true,"title":["極超音速旅客機における時間及びエネルギーに関する最適マッハ数予測"],"weko_creator_id":"2","weko_shared_id":-1},"updated":"2023-06-20T14:33:56.654869+00:00"}