{"created":"2023-06-20T15:11:36.915519+00:00","id":41299,"links":{},"metadata":{"_buckets":{"deposit":"17c9c28a-9dd0-4028-953f-c1c9335f8dd4"},"_deposit":{"created_by":1,"id":"41299","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41299"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041299","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489383","489376","489372","489373","489377","489385","489374","489378","489381","489382","489375","489384","489380","489379"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Research on semi-freejet test method for supersonic jet engine"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"142","bibliographicPageStart":"137","bibliographicVolumeNumber":"45","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_3_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":"20-21 May 1999 (62nd). 25-26 Nov. 1999 (63rd)","subitem_description_type":"Other"}]},"item_3_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":"20-21 May 1999 (62nd). 25-26 Nov. 1999 (63rd)","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"超音速エンジン試験施設の設計に必要なデータを取得するために、小型模型によるセミフリージェット試験法の研究を行った。気流条件は、超音速インテークの2段ランプによる外部圧縮を行った後の状態を模擬したものとした。環境温度が変化することに対応し、温度補償型多点圧力計測装置を使用して、模型各部の圧力分布を測定した。結果として、セミフリージェット方式で超音速飛行時と同等のインテーク流れ場を再現でき、エンジン全体の性能評価ができることを確認した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Research on a semi-freejet test method by using a small model was carried out in order to obtain the data necessary for the design of a supersonic engine test facility. The air flow condition was simulated to the condition after the external compression by a two-stage ramp of supersonic intake. The pressure distribution at each part of the model was measured using a temperature-compensating multiple pressure measurement device, coping with the change in the environmental temperature. As the results, the intake flow field equal to that at a supersonic flight was reproduced by the semi-freejet test method, and the performance evaluation of the whole engine was confirmed to be possible with this test method.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028634014","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 SP-45","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":"0289-260X","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":"AN10097345","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"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"アイ・エヌ・シー・エンジニアリング"}]},"item_3_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"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"INC Engineering Co Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"田口, 秀之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"関根, 静雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"二村, 尚夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"柳, 良二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小見, 淳介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"加藤, 俊樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"寺崎, 眞太郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Taguchi, Hideyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sekine, Shizuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Futamura, Hisao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yanagi, Ryoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Omi, Junsuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kato, Toshiki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Terasaki, Shintaro","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":"nalsp0045014.pdf","filesize":[{"value":"3.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0045014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41299/files/nalsp0045014.pdf"},"version_id":"adbf6adc-4da1-42e4-a9f7-6224b02e1a14"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速ジェットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"セミフリージェット試験","subitem_subject_scheme":"Other"},{"subitem_subject":"気流条件","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速インテーク","subitem_subject_scheme":"Other"},{"subitem_subject":"インテーク流れ場","subitem_subject_scheme":"Other"},{"subitem_subject":"温度補償","subitem_subject_scheme":"Other"},{"subitem_subject":"多点圧力計測","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"シュリーレン像","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波","subitem_subject_scheme":"Other"},{"subitem_subject":"外部圧縮","subitem_subject_scheme":"Other"},{"subitem_subject":"2段ランプ","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"環境温度","subitem_subject_scheme":"Other"},{"subitem_subject":"性能評価","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic jet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"semi freejet test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air flow condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic intake","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"intake flow field","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"temperature compensation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiple pressure measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Schlieren image","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"external compression","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two stage ramp","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"environmental temperature","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"performance evaluation","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":"超音速ジェットエンジン・セミフリージェット試験法の研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速ジェットエンジン・セミフリージェット試験法の研究"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41299","relation_version_is_last":true,"title":["超音速ジェットエンジン・セミフリージェット試験法の研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:03:45.301171+00:00"}