{"created":"2023-06-20T15:07:29.147627+00:00","id":36855,"links":{},"metadata":{"_buckets":{"deposit":"6ce98db5-5d18-4220-a301-13c4e5e7a94d"},"_deposit":{"created_by":1,"id":"36855","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36855"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036855","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477884","477885","477886","477883"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"RCS gas-jet interaction experiment in HYFLEX"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-09","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"150","bibliographicPageStart":"143","bibliographicVolumeNumber":"32","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":"24-25 Jul. 1996","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":"24-25 Jul. 1996","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"姿勢制御用ガスジェット(RCS)と外部流との空力干渉の姿勢制御系へ与える影響を正確に評価することは、極超音速揚力機の設計における重要な技術課題の一つである。そのため、HYFLEX(極超音速飛行実験)においては、主要な空力実験の一つとしてRCSガスジェット干渉に関するデータ取得実験が計画された。本稿では、実験計画の概要について述べるとともに、飛行実験の結果得られた空力干渉データを風洞試験結果と比較しながら示す。比較の結果、HYFLEXの実験計測用ヨーガスジェットの場合には、ジェット一様流に対する運動量比が相関パラメータとして全般的に妥当であることがわかった。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"As experienced in the Space Shuttle orbiter development, estimation of RCS (Reaction Control System) gas-jet interaction effects with external flow is one of key technologies of hypersonic reentry vehicle development. The RCS gas-jet interaction experiment in HYFLEX (Hypersonic Flight Experiment) was planned to establish a method to estimate the interaction effects in flight condition from wind tunnel test results and/or CFD (Computational Fluid Dynamics) calculations. In this paper, flight data on surface pressure distribution around the RCS thrusters in super- to hypersonic speed ranges are presented, being compared with several wind tunnel test results. In the comparison, some jet correlation parameters were examined. As the results, jet momentum ratio to freestream is found to be generally a suitable parameter in the case of the HYFLEX yaw gas-jet thrusters located on the outside surface of stabilizing fins.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000584017","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-32","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":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"渡辺, 重哉"}],"nameIdentifiers":[{"nameIdentifier":"477883","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"高木, 亮治"}],"nameIdentifiers":[{"nameIdentifier":"477884","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Watanabe, Shigeya","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"477885","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Takaki, Ryoji","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"477886","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":"nalsp0032017.pdf","filesize":[{"value":"729.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0032017.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36855/files/nalsp0032017.pdf"},"version_id":"d427fca5-a91e-4a50-ae86-129fc8577356"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速飛行実験","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"RCS","subitem_subject_scheme":"Other"},{"subitem_subject":"リアクションコントロールシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"RCSガスジェット干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD解析","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢制御系","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層剥離","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波","subitem_subject_scheme":"Other"},{"subitem_subject":"ヨー・スラスタ","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flight experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"RCS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reaction control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"RCS gas jet interaction","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":"attitude control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer separation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"yaw thruster","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":"HYFLEXにおけるRCSガスジェット干渉実験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HYFLEXにおけるRCSガスジェット干渉実験"}]},"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":"36855","relation_version_is_last":true,"title":["HYFLEXにおけるRCSガスジェット干渉実験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:30:33.560618+00:00"}