{"created":"2023-06-20T15:07:50.223784+00:00","id":37201,"links":{},"metadata":{"_buckets":{"deposit":"0b15ef8e-1e74-47e1-af5c-edfea0652eb1"},"_deposit":{"created_by":1,"id":"37201","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37201"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037201","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479529","479522","479528","479524","479525","479527","479526","479523"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Diagnosis of air condensation in hypersonic flow"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"228","bibliographicPageStart":"219","bibliographicVolumeNumber":"38","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":"22-23 May 1997 (58th). 27-28 Nov. 1997 (59th)","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":"22-23 May 1997 (58th). 27-28 Nov. 1997 (59th)","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"NAL中型衝撃風洞とRCS(リアクションコントロールサブシステム)試験用ガス混合装置を用いて極超音速流のAir Condensationをピトー圧力波形によって診断する事を試みた。試験は衝撃風洞低圧管作動気体に乾燥空気と水蒸気を含んだ空気を用いて、風洞よどみ点圧力、一様流温度、含有水蒸気量などを変化させAir Condensationに至るピトー圧力波形の変化とOnset Pointを調べた。これらの結果、乾燥空気を用い測定部一様流静温度を変化させた場合の診断はDaumらの試験結果とほぼ一致し、簡便なピトー圧力波形の観測によっても比較的良い精度で気流の診断が行え、また作動気体中の水蒸気の含有量によってはDaumらが示したOnset Pointより安全側でもCondensationに至る事が判明した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Utilizing NAL middle scale shock tunnel and RCS (Reaction Control Subsystem) experimental gas mixing system, diagnosis of air condensation of hypersonic flow by Pitot pressure wave form was attempted. By using dry air and moist air as working gases for low pressure pipe of shock wind tunnel, the change of Pitot pressure wave form to air condensation and the onset point were investigated, varying stagnation pressure of the wind tunnel, temperature of uniform flow and moisture content. From these results, it was clarified that the diagnosis in case of using dry air and changing static temperature of uniform flow at the measuring point was almost the same as the test results by Daum et al. Further, it was found that the air flow diagnosis can be made with comparatively good accuracy by simple measurement of Pitot pressure wave form, and condensation can also occur even in the safety side from onset point as shown by Daum et al. depending on the moisture content of working gas.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001434019","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-38","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"},{"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"},{"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":"山崎, 喬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中北, 和之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"井上, 安敏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"曽我, 国男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamazaki, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakakita, Kazuyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Inoue, Yasutoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Soga, Kunio","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":"nalsp0038019.pdf","filesize":[{"value":"804.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0038019.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37201/files/nalsp0038019.pdf"},"version_id":"06c2b6ab-70e2-4a3a-97f4-651a46a8d744"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"診断","subitem_subject_scheme":"Other"},{"subitem_subject":"空気凝縮","subitem_subject_scheme":"Other"},{"subitem_subject":"ピトー圧力波形","subitem_subject_scheme":"Other"},{"subitem_subject":"よどみ点圧力","subitem_subject_scheme":"Other"},{"subitem_subject":"水蒸気含有量","subitem_subject_scheme":"Other"},{"subitem_subject":"一様流","subitem_subject_scheme":"Other"},{"subitem_subject":"作動気体","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"diagnosis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air condensation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Pitot pressure wave form","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stagnation pressure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"moisture content","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"uniform flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"working gas","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":"極超音速流のAir Condensationの診断","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"極超音速流のAir Condensationの診断"}]},"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":"37201","relation_version_is_last":true,"title":["極超音速流のAir Condensationの診断"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:23:34.601726+00:00"}