{"created":"2023-06-20T15:10:22.293186+00:00","id":39953,"links":{},"metadata":{"_buckets":{"deposit":"e38d2514-c086-496d-9075-61aaa960d0b8"},"_deposit":{"created_by":1,"id":"39953","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39953"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039953","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["445745","445739","445743","445746","445742","445737","445738","445744","445736","445741","445747","445740"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A pressure test of RCS jet interference at a Mach number of 5 for a tip fin configuration"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"13","bibliographicPageStart":"1","bibliographicVolumeNumber":"714","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":"RCS(Reaction Control System:ガスジェット姿勢制御システム)ガスジェット干渉圧力試験を出口径φ50cmの航技研極超音速風洞で行った。ティップフィンを持つ01HOPEb(HOPE:H-2ロケット打上げ型有翼回収機)形状1.2%模型を使用し、常温の乾燥空気およびアルゴンを用いてヨージェットを模擬した。主流マッハ数は5.05、試験迎角は16度、23度、30度、33度である。機体表面圧力分布を測定し、油膜法による流れの可視化を行った。低迎角ではジェットノズル付近で胴体周りの流れの剥離がみられ、高迎角ではジェットプルームがティップフィンを含む翼面上に直接影響をおよぼすことが分った。圧力積分結果より、ヨー方向の干渉モーメントがラダー効きに匹敵すること、また迎角、ジェット比熱比が異なっても、動圧比に面積比を乗じた運動量比で干渉力の相関が取れることが分った。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Aerodynamic interference induced by a Reaction Control System (RCS) jet was investigated for a tip fin configuration at a Mach number of 5. Surface pressure distributions and oil-flow photographs were obtained using cold gas simulation techniques with yaw jet scaled nozzles in the NAL phi 50 cm hypersonic wind tunnel. It was found that the interference flow field changed as angles of attack and jet parameters changed. Pressure summation results showed that induced yawing moments became comparable to rudder effectiveness. Aerodynamic interference forces were correlated with momentum ratio as the angle of attack and the specific heat ratio of the jet changed.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001069000","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-714","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 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"永井, 伸治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"穂積, 弘一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉沢, 昭"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"原, 亘利"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石田, 清道"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤井, 啓介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagai, Shinji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hozumi, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshizawa, Akira","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hara, Nobutoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishida, Kiyomichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujii, Keisuke","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":"naltm0000714.pdf","filesize":[{"value":"332.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm0000714.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39953/files/naltm0000714.pdf"},"version_id":"8a5ce98f-111b-4e97-bae1-9625f81ff284"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2ロケット打上げ型有翼回収機","subitem_subject_scheme":"Other"},{"subitem_subject":"ティップフィン形態","subitem_subject_scheme":"Other"},{"subitem_subject":"RCS","subitem_subject_scheme":"Other"},{"subitem_subject":"ガスジェット姿勢制御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"ガスジェット干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"空力干渉圧力試験","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"表面圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"油膜法可視化","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層剥離","subitem_subject_scheme":"Other"},{"subitem_subject":"ジェットプルーム","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"tip fin configuration","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":"gas jet interference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic interference pressure test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"surface pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"oil film method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer separation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"jet plume","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":"マッハ5におけるティップフィン形態のRCSジェット干渉圧力試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"マッハ5におけるティップフィン形態のRCSジェット干渉圧力試験"}]},"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":"39953","relation_version_is_last":true,"title":["マッハ5におけるティップフィン形態のRCSジェット干渉圧力試験"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:18:03.434237+00:00"}