{"created":"2023-06-20T15:07:59.384132+00:00","id":37372,"links":{},"metadata":{"_buckets":{"deposit":"6dde85a4-ffdf-405b-8e55-ad535e075cc1"},"_deposit":{"created_by":1,"id":"37372","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37372"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037372","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480408","480410","480411","480409"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"CFD analysis of transonic and supersonic flow around HOPE for aerodynamic design"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"366","bibliographicPageStart":"361","bibliographicVolumeNumber":"41","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 24-26 Jun. 1998 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 24-26 Jun. 1998 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"HOPE-X(宇宙往還技術試験機)回りのナビエ・ストークス流の計算を行い、その空力設計のための有用なデータを多く得た。本報では、流れの計算に対して2種類の比較調査を行った。最初は、コード間の比較を行い、CFD(数値流体力学)コードの信頼性を試験した。ここに使用されている2つのCFDコードは、両方とも、TVD(全変動減少)風上スキームを持つ有限体積法で分割された薄層近似レイノルズ平均ナビエ・ストークス方程式を基礎としている。これらのコードによって得られた結果は10度以下の迎角でお互いに良い一致を見せた。第2番目は、1つのCFDコードで2つの異なる格子について流れの計算を行い、コードの格子依存性を推定した。格子依存性は小さく、空力設計にこのCFDコードが充分使用できる。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Navier-Stokes flow simulations around HOPE-X (H-2 Orbiting Plane Experimental) have been carried out to yield various useful data for its aerodynamic design. In this paper, two kinds of validation studies for the flow simulations are reported. First, the code to code validation was executed to test the reliability of the CFD (Computational Fluid Dynamics) codes. The two CFD codes used here are both based on the Reynolds averaged thin layer approximated Navier-Stokes equations which are made discrete by the finite volume method with a TVD (Total Variation Diminishing) upwind scheme. The results obtained by these codes are in good agreement with each other at angle of attack lower than ten degrees. Second, flow simulations by one CFD code with different two grids were executed to estimate the grid dependence of the code. Grid dependence is small enough to use the CFD code for aerodynamic design.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001958058","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-41","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":"nalsp0041058.pdf","filesize":[{"value":"508.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0041058.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37372/files/nalsp0041058.pdf"},"version_id":"50dacd1b-dc7f-4581-aa30-14d3f759d7c0"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"宇宙往還技術試験機","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE-X","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"空力設計","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"TVDスキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"有限体積法","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"全変動減少スキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane Experimental","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE X","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TVD scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"finite volume method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"total variation diminishing scheme","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の遷・超音速流空力設計CFD解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HOPEの遷・超音速流空力設計CFD解析"}]},"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":"37372","relation_version_is_last":true,"title":["HOPEの遷・超音速流空力設計CFD解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:20:37.359182+00:00"}