{"created":"2023-06-20T15:07:29.627200+00:00","id":36862,"links":{},"metadata":{"_buckets":{"deposit":"3d00b7e4-6f5a-46b2-a5da-3bf124086b35"},"_deposit":{"created_by":1,"id":"36862","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36862"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036862","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477912","477911"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Higher-order shock-vortex capturing for unsteady internal and external flows"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"18","bibliographicPageStart":"13","bibliographicVolumeNumber":"34","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 6-7 JUN. 1996 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 6-7 JUN. 1996 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"衝撃波と渦を含む幾つかの複雑な非定常流れの問題を数値的に検討した。空間差分における高解像度衝撃波捕獲スキームは有効近似リーマン解法と結びついている4次コンパクトMUSCL-TVD(Monotonic Upstream Scheme for Conservation Laws-Total Variation Diminishing)スキームに基づいており、研究で用いた数値解法は、このスキームと最大2次精度陰的スキームから成立っている。幾つかの代表的計算結果を示した。第一の事例は、タービンカスケードトンネルを通る非定常遷音速流問題である。第二の事例は、高迎角のNACA翼周りの非定常遷音速流、第三の事例は、タイプ4衝撃波加熱問題として知られている非定常超音速衝撃波/衝撃波干渉流である。また、衝撃波渦捕獲法の信頼性を論じた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Some complicated unsteady flow problems involving not only shocks, but vortices are numerically investigated. Numerical methods employed in the present research are composed of the higher-resolution shock capturing schemes in space difference based on the fourth-order compact MUSCL (Monotonic Upstream Schemes for Conservation Laws) TVD (Total Variation Diminishing) scheme coupled with an efficient approximate Riemann solver, and the maximum second-order accurate implicit schemes. Some typical calculated results are shown. The first case is the unsteady transonic flow problem through a turbine cascade tunnel. The second case is the unsteady transonic flow around NACA airfoil at high angle of attack, and the third case is unsteady hypersonic shock/shock interference flow known as the Type 4 shock heating problem. Finally, the reliability of so-called the shock-vortex capturing method is discussed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000685003","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-34","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":"東北大学 大学院"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山本, 悟"}],"nameIdentifiers":[{"nameIdentifier":"477911","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Yamamoto, Satoru","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"477912","nameIdentifierScheme":"WEKO"}]}]},"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":"nalsp0034003.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0034003.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36862/files/nalsp0034003.pdf"},"version_id":"43a0ae20-a4e1-444b-aa2b-ab4e8df55e19"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"非定常流","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解法","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波渦捕獲","subitem_subject_scheme":"Other"},{"subitem_subject":"空間差分","subitem_subject_scheme":"Other"},{"subitem_subject":"近似リーマン解法","subitem_subject_scheme":"Other"},{"subitem_subject":"MUSCL-TVDスキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"高次精度スキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速衝撃波","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock vortex capturing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space difference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"approximate Riemann solver","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"MUSCL TVD scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high order accurate scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic shock wave","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":"非定常圧縮性流れの高解像度衝撃波/渦捕獲法","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"非定常圧縮性流れの高解像度衝撃波/渦捕獲法"}]},"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":"36862","relation_version_is_last":true,"title":["非定常圧縮性流れの高解像度衝撃波/渦捕獲法"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:30:25.990167+00:00"}