{"created":"2023-06-20T15:10:43.258451+00:00","id":40296,"links":{},"metadata":{"_buckets":{"deposit":"af3ac1f3-aecc-49f5-b700-c4df2e96d921"},"_deposit":{"created_by":1,"id":"40296","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40296"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040296","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["447149","447148","447145","447147","447144","447146"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Application of Navier-Stokes CFD code FIVAD to structural heat conduction problems"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"11","bibliographicPageStart":"1","bibliographicVolumeNumber":"729","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"圧縮製ナビエ・ストークスCFD(計算流体力学)コードFIVADが空力加熱と連成した機体伝熱問題のシミュレーションに利用されている。FIVADの用いるAUSMDVスキームなどの基礎理論式、実際のコードの特徴と構造、および機体伝熱問題との連成計算への応用例を示す。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A compressive Navier-Stokes CFD (Computational Fluid Dynamics) code FIVAD is currently utilized for numerical simulation of heat conduction problems under aerodynamic heating. In this paper the governing equations and its characteristics of AUSMDV scheme, which is used in FIVAD, are described, then the structures of the code are shown and finally some computational results of test problems are presented.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001656000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TM-729","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0452-2982","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00314334","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 構造力学部"},{"subitem_text_value":"航空宇宙技術研究所 構造力学部"},{"subitem_text_value":"航空宇宙技術研究所 数理解析部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structural Mechanics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structural Mechanics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Computational Sciences Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"高崎, 浩一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大竹, 邦彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小川, 哲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takasaki, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Otake, Kunihiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ogawa, Satoru","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":"2020-01-27"}],"displaytype":"detail","filename":"naltm0000729.pdf","filesize":[{"value":"334.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm0000729.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40296/files/naltm0000729.pdf"},"version_id":"24e3bf6a-15df-42e6-8250-3c0455993b0d"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"機体熱伝導","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーションコード","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮性流","subitem_subject_scheme":"Other"},{"subitem_subject":"表面熱流束","subitem_subject_scheme":"Other"},{"subitem_subject":"機体構造","subitem_subject_scheme":"Other"},{"subitem_subject":"FIVAD","subitem_subject_scheme":"Other"},{"subitem_subject":"大気圏再突入","subitem_subject_scheme":"Other"},{"subitem_subject":"2次元円柱","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙飛行体","subitem_subject_scheme":"Other"},{"subitem_subject":"airframe heat conduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressible flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"surface heat flux","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airframe structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"FIVAD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"atmosphere reentry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional cylinder","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"圧縮性NSコードFIVADの機体伝熱問題に対する応用について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"圧縮性NSコードFIVADの機体伝熱問題に対する応用について"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"40296","relation_version_is_last":true,"title":["圧縮性NSコードFIVADの機体伝熱問題に対する応用について"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:16:14.073762+00:00"}