{"created":"2023-06-20T15:08:00.182558+00:00","id":37388,"links":{},"metadata":{"_buckets":{"deposit":"c7d7916e-8013-492e-adf0-8e3242cb2c5c"},"_deposit":{"created_by":1,"id":"37388","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37388"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037388","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480516","480515","480523","480521","480522","480514","480520","480517","480518","480519"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A comparison test on aerodynamic heating around 09HOPE in NAL hypersonic wind tunnel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"79","bibliographicPageStart":"61","bibliographicVolumeNumber":"42","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"21-22 May 1998 (60th). 26-27 Nov. 1998 (61st)","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"21-22 May 1998 (60th). 26-27 Nov. 1998 (61st)","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"現在設計が進められている有翼宇宙往還機HOPE-Xの空力加熱データ取得の目的でNASDA発注により1996年および1997年にAEDC(アーノルド工学開発センター)VKF(フォン・カルマン空気力学施設)風洞B、Cにおいて試験が実施されていた。今回これらとの対応風試を航技研極超音速風洞において行ったのでそれらの結果の比較について報告する。模型は基準長576mmの3.6%HOPE(H-2ロケット打ち上げ型有翼回収機)であって、今回の風試では表面上のおよそ400個所に埋め込まれた加熱率センサの一部を用いて空力加熱を計測した。AEDCにおいて行われたケースに完全に対応したデータは必ずしも得られていないが、14Run、43ケースの試験を行った。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"To obtain the aerodynamic heating data of HOPE-X (H-2 Orbiting Plane Experimental), the design of which is now in progress, experiments placed by NASDA were performed at AEDC (Arnold Engineering Development Center) VKF (Von Karman gas dynamics Facility) tunnel B, C in 1996 and 1997. A comparison test has been performed at the NAL hypersonic wind tunnel and the results are reported here. The model is a 3.6 percent HOPE (H-2 Orbiting Plane) of the reference length 576 mm. In the experiment, the aerodynamic heating is measured by about 400 heating rate sensors embedded on the surface of the model. Although the data are not completely corresponding to the AEDC case, 14 runs of 43 cases of experiments have been performed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001959008","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-42","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"宇宙開発事業団"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"藤井, 啓介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"穂積, 弘一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"津田, 尚一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小山, 忠勇"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"若松, 逸雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujii, Keisuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hozumi, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsuda, Shoichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koyama, Tadao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wakamatsu, Itsuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0042008.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0042008.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37388/files/nalsp0042008.pdf"},"version_id":"59028450-c47d-430a-905a-ecd7f295fecd"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HOPE-X","subitem_subject_scheme":"Other"},{"subitem_subject":"09HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙往還技術試験機","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"対応風試","subitem_subject_scheme":"Other"},{"subitem_subject":"AEDC","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"加熱率センサ","subitem_subject_scheme":"Other"},{"subitem_subject":"大気圏再突入","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"アーノルド工学開発センター","subitem_subject_scheme":"Other"},{"subitem_subject":"VKF","subitem_subject_scheme":"Other"},{"subitem_subject":"フォン・カルマン空気力学施設","subitem_subject_scheme":"Other"},{"subitem_subject":"迎角効果","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE X","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"09HOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane Experimental","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"comparison test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"AEDC","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heating rate sensor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"atmosphere reentry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Arnold Engineering Development Center","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"VKF","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Von Karman gas dynamics Facility","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attack angle","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":"航技研極超音速風洞における09HOPE熱対応風試について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航技研極超音速風洞における09HOPE熱対応風試について"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37388","relation_version_is_last":true,"title":["航技研極超音速風洞における09HOPE熱対応風試について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:20:12.349580+00:00"}