{"created":"2023-06-20T15:08:03.776086+00:00","id":37451,"links":{},"metadata":{"_buckets":{"deposit":"2d82e12e-badd-4367-a90f-ddb513d043ce"},"_deposit":{"created_by":1,"id":"37451","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37451"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037451","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480849","480850"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"CFD contribution to development of HYPR90"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"119","bibliographicPageStart":"117","bibliographicVolumeNumber":"44","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 16-18 Jun. 1999 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 16-18 Jun. 1999 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"超音速輸送機における推進システムの技術実証のため、HYPR(超音速輸送機用推進システム)プロジェクトにける3形態のサブスケール試作エンジン、すなわち、HTCE(超高温コアエンジン)、HYPR90-T(ターボファンジェットエンジン)、HYPR90-C(コンバインサイクルエンジン)を用いて、テストが行われた。CFD(数値流体力学)を用いた模擬は、エンジンテストにおいて達成されるであろう期待性能を確認するための部品設計を評価するために、また、試験で観測された現象の理解を助けるために、導入されてきた。この論文では、以下のCFDの適用例を紹介する。すなわち、燃焼器からのホットストリーク流入を考慮した単段高圧タービンの3次元非定流体解析、高圧圧縮機内ディスクキャビティの定常軸対称流体解析、排出ガイド翼のついたリム後方キャビティの3次元流体解析、高圧タービンのタービンディスクキャビティの3次元定常流体解析である。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Tests using three prototype sub-scale engines in HYPR (Super/Hyper sonic Transport Propulsion System) project (HTCE (High Temperature Core Engine), HYPR90-T (Turbofan jet engine) and HYPR90-C (Combined cycle engine) ) were conducted to verify the technologies for the propulsion system of a hypersonic transport. Simulations using CFD (Computational Fluid Dynamics) were introduced to assess the component design to make sure that the intended performance would be achieved in the engine tests, and to support the interpretation of phenomena observed in the tests. In this paper, the following examples of the CFD applications are shown: three dimensional unsteady flow analyses of a single stage high pressure turbine including hot streaks from combustion cambers, axisymmetric steady flow analyses around disc cavities of a high pressure compressor, three dimensional flow analyses of a rim rear cavity with exit guide vanes and three dimensional steady flow analyses of turbine disc cavity of high pressure turbine.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001961018","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-44","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":"石川島播磨重工業"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Ishikawajima Harima Heavy Industries Co ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"児玉, 秀和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kodama, Hidekazu","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":"nalsp0044018.pdf","filesize":[{"value":"752.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0044018.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37451/files/nalsp0044018.pdf"},"version_id":"ea83e8aa-face-4620-a8f0-fbced8fac599"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HYPR","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速輸送機用推進システム","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"ターボファンジェットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"コンバインサイクルエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"超高温コアエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常流体解析","subitem_subject_scheme":"Other"},{"subitem_subject":"定常流体解析","subitem_subject_scheme":"Other"},{"subitem_subject":"キャビティ","subitem_subject_scheme":"Other"},{"subitem_subject":"HYPR","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"super hyper sonic transport propulsion system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbofan jet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combined cycle engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high temperature core engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"steady flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cavity","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":"HYPR90開発におけるCFDの適用","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HYPR90開発におけるCFDの適用"}]},"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":"37451","relation_version_is_last":true,"title":["HYPR90開発におけるCFDの適用"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:18:34.804102+00:00"}