{"created":"2023-06-20T15:08:04.189922+00:00","id":37457,"links":{},"metadata":{"_buckets":{"deposit":"5df68efe-43ea-4647-b1f5-7df4d5d49354"},"_deposit":{"created_by":1,"id":"37457","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37457"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037457","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480880","480878","480879","480877"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Navier-Stokes numerical simulations of transonic flows about HOPE with elevons"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"166","bibliographicPageStart":"161","bibliographicVolumeNumber":"44","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 16-18 Jun. 1999 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 16-18 Jun. 1999 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"宇宙往還技術試験機の空力設計を支援するため、数々のHOPE-X(宇宙往還技術試験機)に関する流れのシミュレーションが行われている。空力特性を詳細に調べるために、エルボンが20度下げの状態におけるHope-Xまわりの遷音速流の予備的な解析を行った。この計算では、TVD(全変動減少)風上差分スキームによるFVM(有限体積法)を使って差分化したレイノルズ平均ナビエ・ストークス方程式を基にしたCFDコードを用いた。計算に用いた計算格子は、42ブロックからなるマルチブロック格子である。全格子点の数は、約370万であった。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A large number of flow simulations about HOPE-X (H-2 Orbiting Plane Experimental) has been carried out to support its aerodynamic design. In order to investigate the aerodynamic characteristics in detail, preliminary computations of transonic flows about HOPE-X with -20-degree steered elevons were executed. The CFD (Computational Fluid Dynamics) code used here is based on Reynolds averaged Navier-Stokes equations discretely divided using FVM (Finite Volume Method) method with TVD (Total Variation Diminishing) upwind scheme. The computational grid used here is multi block structured one consisting of 42 blocks. Total number of the grid-points is about 3.7 millions.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001961024","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-44","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":"大興電子通信"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Daiko Denshi Tsushin Ltd"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"伊藤, 良三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 行光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Ryozo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Yukimitsu","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":"nalsp0044024.pdf","filesize":[{"value":"3.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0044024.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37457/files/nalsp0044024.pdf"},"version_id":"00e1ab56-10dd-4022-beef-88da1d915845"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HOPE-X","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙往還技術試験機","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"TVDスキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"全変動減少スキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"エレボン","subitem_subject_scheme":"Other"},{"subitem_subject":"ボルドウィン-ローマックス乱流モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"マルチブロック格子","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE X","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":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TVD scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"total vibration diminishing scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"elevon","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Baldwin Lomax turbulent flow model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multi block grid","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エレボン操舵形態周りの遷音速流Navier-Stokes数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HOPEエレボン操舵形態周りの遷音速流Navier-Stokes数値シミュレーション"}]},"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":"37457","relation_version_is_last":true,"title":["HOPEエレボン操舵形態周りの遷音速流Navier-Stokes数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:18:27.172917+00:00"}