{"created":"2023-06-20T15:07:24.121224+00:00","id":36772,"links":{},"metadata":{"_buckets":{"deposit":"0df22be8-2820-45a8-b150-9d165846a96c"},"_deposit":{"created_by":1,"id":"36772","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36772"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036772","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477520","477524","477523","477519","477522","477521"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Application and role of numerical simulation of hypersonic flow for the development of HOPE (H-2 Orbiting Plane)"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"22","bibliographicPageStart":"17","bibliographicVolumeNumber":"30","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":"航空宇宙技術研究所 7-9 Jun. 1995 東京 日本","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":"National Aerospace Laboratory 7-9 Jun. 1995 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"HOPE(H-2ロケット打ち上げ型有翼宇宙往環機)周りの極超音速流を流速分割および流速差分分割風上TVD Navier-Stokesコードを用いて数値解析した。2タイプの候補形状設計から基本形態を決めるために新しいパラメータ計算を行った。1つはダブルデルタタイプ(DDモデル)で、他の1つはパワーデルタタイプ(PDモデル)である。また、実在気体効果の調査研究のためDLR,HEG(Goettingenの高エンタルピー衝撃風洞)およびCaltech T-5の高エンタルピー風洞の流れ条件に対応した数値計算を行った。さらに、AEDCおよびONERA S4MAの極超音速風洞とCalspanの衝撃風洞の各試験との比較対応のための数値計算も行った。これらの数値解析を通じて、HOPEの空力・空力加熱特性の詳細を究明できた。本研究はNALとNASDAの共同で実施された。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Numerical study of hypersonic flow around HOPE is performed, using flux-split and flux difference splitting upwind TVD (Total Variation Diminishing) Navier-Stokes codes. New parametric computations are made to determine the basic configuration from two type of HOPE candidate geometry designs. One type is the Double Delta type model (DD model) and the other is the Power Delta type one (PD model). Also, in order to investigate real gas effects, numerical calculations, corresponding to the flow conditions of high enthalpy wind tunnels of DLR, HEG (High Enthalpy Shock Tunnel Goettingen) and Caltech (California Institute of Technology) T-5, are made. In addition, hypersonic perfect gas flow calculations are made for the comparison with experimental data of AEDC (Arnold Engineering Development Center) and ONERA S4MA hypersonic wind tunnel and Calspan's shock Tunnel. Through the present numerical analysis, detailed aerodynamic and aerothermodynamic characteristics of HOPE are investigated. These works have been done as the joint research of NAL and NASDA.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000294004","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-30","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":"富士通"}]},"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":"Fujitsu Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山本, 行光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"和田, 安弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉岡, 美菜子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Yukimitsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wada, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshioka, Minako","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":"nalsp0030004.pdf","filesize":[{"value":"646.1 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0030004.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36772/files/nalsp0030004.pdf"},"version_id":"b340d90f-5ac6-4f08-9967-e72b03d8036a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"H-2ロケット打ち上げ型有翼宇宙往環機","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"流速分割","subitem_subject_scheme":"Other"},{"subitem_subject":"流速差分分割","subitem_subject_scheme":"Other"},{"subitem_subject":"風上TVDNavier-Stokesコード","subitem_subject_scheme":"Other"},{"subitem_subject":"高エンタルピー風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"デルタ翼","subitem_subject_scheme":"Other"},{"subitem_subject":"実在気体効果","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"H2 orbiting space plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flux split","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flux difference split","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"finite difference method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"upwind TVD Navier Stokes code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"delta wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"real gas effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating","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":"HOPE開発における超高速流数値シミュレーション技術の応用とその役割","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HOPE開発における超高速流数値シミュレーション技術の応用とその役割"}]},"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":"36772","relation_version_is_last":true,"title":["HOPE開発における超高速流数値シミュレーション技術の応用とその役割"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:31:58.175669+00:00"}