{"created":"2023-06-20T15:13:26.931992+00:00","id":43377,"links":{},"metadata":{"_buckets":{"deposit":"24649fe8-710e-4c38-8c88-834f1648d21e"},"_deposit":{"created_by":1,"id":"43377","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43377"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043377","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["463499","463495","463498","463500","463497","463496"],"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 Flow Around H-II Orbiting Plane"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1989-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"302","bibliographicPageStart":"295","bibliographicVolumeNumber":"10","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 SP-10","bibliographic_titleLang":"en"}]}]},"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) has been studied by National Space Development Agency of JAPAN (NASADA). The gross weight is planned about 9.O tons at launch with the payload of about 1.2 tons. The current baseline configuration of the HOPE has a double delta wing with tip fins. The double delta type wing planform is expected to have smaller longitudinal trim change over all the flight regions and tip fins are adopted in order to gain easier access to Space Station or other platforms than the vertical tail wings on the fuselage. 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 lateral and directional aerodynamic characteristics. This work has been done as the joint research of National Aerospace Laboratory (NAL) and NASDA. Numerical computations were carried out at M infinity =7.0 and Reynolds number of 2.5 by 106 at angles of attack 0, 20 and 40 degrees with yaw angle of 5 deg. Numerical results were compared with experimental data obtained from hypersonic wind tunnel (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: NALSP0010048","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 SP-10","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":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_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_3_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":"宇宙開発事業団"},{"subitem_text_value":"AES Inc"}]},"item_3_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 Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"AES Inc."}]},"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":"鈴木, 尚行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Yukimitsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Akimoto, Toshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Naoyuki","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":"2020-01-28"}],"displaytype":"detail","filename":"nalsp0010048.pdf","filesize":[{"value":"988.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0010048.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43377/files/nalsp0010048.pdf"},"version_id":"670e7845-7f56-407e-84a0-1df3c9abe698"}]},"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まわりの極超音流数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HOPEまわりの極超音流数値シミュレーション"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43377","relation_version_is_last":true,"title":["HOPEまわりの極超音流数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:16:09.989553+00:00"}