{"created":"2023-06-20T15:08:23.546170+00:00","id":37829,"links":{},"metadata":{"_buckets":{"deposit":"153e86a6-6706-465b-812c-8906d6d9985f"},"_deposit":{"created_by":1,"id":"37829","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37829"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037829","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["430509","430507","430508","430505","430510","430506"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Hypersonic Navier-Stokes simulations around OREX"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"39","bibliographicPageStart":"35","bibliographicVolumeNumber":"26","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_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"軸対称ナビエ･ストークス方程式を解くことにより、マッハ数7.1の空気の流れの中におけるOREXのまわりの流れの数値シミュレーションを行った。強い衝撃波と膨張波が生成され相互に干渉し合う領域で誤差が集積することのないよう数値解法にはvan Leerの流束分割法を修正したHaenelの分割法を採用した。また高精度解法として有限容積法に対しTVD-MUSCL法を適用した。時間積分には2段階のルンゲ･クッタ法を用いた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Numerical simulations of the flows around Orbital Reentry Experiment (OREX) has been performed in a Mach 7.1 air stream by solving axisymmetric Navier-Stokes equations. Haenel's Flux Vector Splitting, which is a modified form of the original van Leer's splitting, is adopted to the numerical method in order to avoid an accumulated error appearing in the regions where strong shock and expansion waves are generated and interact with each other. Additionally, the TVD-MUSCL (Total Variation Diminishing-Monotone Upstream-centered Scheme for Conservation Laws) approach is applied to the finite volume method as a high resolution scheme. The two-step Runge-Kutta method is used for time integration.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004173005","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-26","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":"日立製作所 機械研究所"},{"subitem_text_value":"日立製作所 機械研究所"},{"subitem_text_value":"日立製作所 機械研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Hitachi Ltd Mechanical Engineering Research Laboratory"},{"subitem_text_language":"en","subitem_text_value":"Hitachi Ltd Mechanical Engineering Research Laboratory"},{"subitem_text_language":"en","subitem_text_value":"Hitachi Ltd Mechanical Engineering Research Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"瀬川, 清"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中野, 晋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"坪内, 邦良"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Segawa, Kiyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakano, Susumu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsubouchi, Kuniyoshi","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":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0026005.pdf","filesize":[{"value":"425.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0026005.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37829/files/nalsp0026005.pdf"},"version_id":"f7f0d85c-d7a3-407e-a89a-011b2807efb8"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"非平衡流","subitem_subject_scheme":"Other"},{"subitem_subject":"実在気体効果","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD解析","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ･ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"OREX","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道再突入実験","subitem_subject_scheme":"Other"},{"subitem_subject":"流速ベクトル分割","subitem_subject_scheme":"Other"},{"subitem_subject":"人工粘性項制御","subitem_subject_scheme":"Other"},{"subitem_subject":"数値不安定","subitem_subject_scheme":"Other"},{"subitem_subject":"粘性衝撃層解析","subitem_subject_scheme":"Other"},{"subitem_subject":"非平衡粘性衝撃層","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nonequilibrium flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"real gas effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equations","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"OREX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbital reentry experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flux vector splitting","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"artificial viscosity control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical instability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"viscous shock layer analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nonequilibrium viscous shock layer","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":"OREXまわりの極超音速ナビエ･ストークス解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"OREXまわりの極超音速ナビエ･ストークス解析"}]},"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":"37829","relation_version_is_last":true,"title":["OREXまわりの極超音速ナビエ･ストークス解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:48:42.603308+00:00"}