{"created":"2023-06-20T15:15:13.681618+00:00","id":45287,"links":{},"metadata":{"_buckets":{"deposit":"f6619561-fef7-4507-a0c4-14a272f0fcda"},"_deposit":{"created_by":1,"id":"45287","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45287"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045287","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["473887","473888","473886","473885"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical Simulation of Hypersonic Viscous Flow for the Design of H-II Orbiting Plane (HOPE)"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1989-08","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"98","bibliographicVolumeNumber":"1028","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1028","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所と宇宙開発事業団との共同研究「H-IIロケット打上げ型有翼宇宙往還機(HOPE)の研究」の一環として,昭和62年度から昭和63年度にかけて行われた空力特性の研究のうち,極超音速領域の空力数値解析に関する成果を報告する。数値解析はナビエ・ストークス方程式を用いて,マッハ数7.0,全長を基準にしたレイノルズ数2.5×10(exp 6)で,迎角は0度から40度,横すべり角0度,及び5度の条件で,三種類のHOPEオービタ形状について行った。数値計算結果を当所極超音速風洞における実験結果との比較を行い,空力係数については良好な一致を得た。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An unmanned winged vehicle for space transportation called H-II Orbiting Plane (HOPE)is being studied by the National Space Development Agency of JAPAN (NASDA). In the present paper, hypersonic computational fluid dynamics (CFD) analyses have been performed for the 62A, 62B, and 62C HOPE configurations in order to investigate aerodynamic and aerothermodynamic characteristics. This research has been carried out jointly by the National Aerospace Laboratory (NAL) and NASDA. Numerical computations were carried out at M∞=7.0 and Reynolds number of 2.5×10(exp 6) at angles of attack from 0, to 40 degrees with and without yaw angles. Numerical results were compared with experimental data obtained from the hypersonic wind tunnnel(HWT) at NAL.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1028000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-1028","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所空気力学部"},{"subitem_text_value":"宇宙開発事業団"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aerodynamics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan(NASDA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山本, 行光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"秋元, 敏男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"YAMAMOTO, Yukimitsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"AKIMOTO, Toshio","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr01028.pdf","filesize":[{"value":"7.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01028.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45287/files/naltr01028.pdf"},"version_id":"b0982b0b-e90e-4a84-979e-e50964193920"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"HOPEの極超音速空力数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HOPEの極超音速空力数値シミュレーション"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"45287","relation_version_is_last":true,"title":["HOPEの極超音速空力数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:42:00.762958+00:00"}