{"created":"2023-06-20T15:07:23.626618+00:00","id":36762,"links":{},"metadata":{"_buckets":{"deposit":"c2c019c1-7b2e-4cdf-90e2-09c2278c0192"},"_deposit":{"created_by":1,"id":"36762","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36762"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036762","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477477","477476","477475","477474"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"OREXおよび双曲面フレア回りの極超音速流解析"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"139","bibliographicPageStart":"134","bibliographicVolumeNumber":"29","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 8 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 8 Jun. 1995 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"軸対象ナビエ・ストークス方程式を解いてOREX(軌道再突入実験)および双曲面フレア回りの極超音速流解析を行った。この流れの解法は、有限体積陰的全変動減少(TVD)風上スキームに基づいている。対流束は、“カーバンクル現象”を除くためにAUSM(移動上流分割法)DVスキームで評価した。これは鈍頭体回りの極超音速流れの解析によく見かける非物理的解法である。また平衡空気の熱力学的および輸送特性を推定するのに曲線あてはめを採用した。OREXの流れの状態は、高度56.9kmでの飛行条件に対応しており、そこでは実在気体効果が無視されることはない。それ故に、この流れは完全気体であるばかりでなく平衡気体であると想定した。双曲面フレアの場合、流れの状態は低温気体を使用するGottingenのLudwigチューブでの実験に対応している。この課題の数値解析結果は、衝撃波と境界層間の相互作用によって引き起こされる分離を含む極超音速流の空気力学および空気熱力学特徴を正確に予測するために、流れの非定常性を考慮しなければならないことを示唆している。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Hypersonic flow analysis around OREX (Orbiter Reentry Experiment) and hyperboloid flare have been carried out by solving axisymmetric Navier-Stokes equations. The flow solver is based on a finite volume implicit TVD (Total Variation Diminishing) upwind scheme. Convective fluxes are evaluated by AUSM (Advection Upstream Splitting Method) DV scheme in order to remove carbuncle phenomena, that are unphysical solution often appeared on hypersonic flow analysis around a blunt body. A curve fitting were also adopted to estimate thermodynamic and transport properties of an equilibrium air. Flow condition for OREX corresponds to a flight condition at altitude 56.9 km, where real gas effect should not be ignored. Therefore, it was assumed that this flow was not only to be a perfect gas, but also to be an equilibrium air. In the case of hyperboloid flare, flow condition corresponds to experiment by Gottingen Ludwig tube used cold gas. Numerical result of this problem suggests that the flow unsteadiness must be taken into account, in order to predict accurately the aerodynamic and aerothermodynamic characteristics of a hypersonic flow including separations induced by the interaction between a shock wave and boundary layer.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000110012","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-29","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":"川崎重工業 岐阜技術研究所"},{"subitem_text_value":"川崎重工業 航空宇宙事業本部　航空宇宙事業部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd Gifu Technical Institute"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd Aerospace Engineering Division, Space Project Engineering Department"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"岸本, 琢司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"金子, 進一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kishimoto, Takuji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kaneko, Shinichi","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":"nalsp0029012.pdf","filesize":[{"value":"382.1 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0029012.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36762/files/nalsp0029012.pdf"},"version_id":"76bf19d6-8135-4c93-b3ca-fc89217d3906"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"OREX","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道再突入実験","subitem_subject_scheme":"Other"},{"subitem_subject":"双曲面フレア","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速流解析","subitem_subject_scheme":"Other"},{"subitem_subject":"TVD","subitem_subject_scheme":"Other"},{"subitem_subject":"全変動減少","subitem_subject_scheme":"Other"},{"subitem_subject":"対流束","subitem_subject_scheme":"Other"},{"subitem_subject":"鈍頭体","subitem_subject_scheme":"Other"},{"subitem_subject":"カーバンクル現象","subitem_subject_scheme":"Other"},{"subitem_subject":"AUSM","subitem_subject_scheme":"Other"},{"subitem_subject":"移送上流分離方式","subitem_subject_scheme":"Other"},{"subitem_subject":"平衡空気","subitem_subject_scheme":"Other"},{"subitem_subject":"高エンタルピー流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"軸対象ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"流れの非定常性","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":"hyperboloid flare","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TVD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"total variation diminishing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"convective fluxes","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"blunt body","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"carbuncle phenomena","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"AUSM","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"advection upstream splitting method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"equilibrium air","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high enthalpy flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"axisymmetric Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow unsteadiness","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Hypersonic flow analysis around OREX and hyperboloid flare","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Hypersonic flow analysis around OREX and hyperboloid flare","subitem_title_language":"en"}]},"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":"36762","relation_version_is_last":true,"title":["Hypersonic flow analysis around OREX and hyperboloid flare"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:32:13.015557+00:00"}