{"created":"2023-06-20T15:07:49.841674+00:00","id":37195,"links":{},"metadata":{"_buckets":{"deposit":"8f35212d-5cae-4f22-b9ac-e1cbcfec5982"},"_deposit":{"created_by":1,"id":"37195","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37195"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037195","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479480","479483","479484","479487","479482","479486","479485","479481","479478","479479"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"High speed characteristic test of an ADS probe with multi hole pyramidal head"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"165","bibliographicPageStart":"155","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":"SST(超音速輸送機)およびHOPE(H-2ロケット打上げ型有翼回収機)のエアデータシステム(ADS)の研究開発を目的として、NALはプローブ(ピトー管およびボディーヘッド型)の高速特性試験を実施した。 NALの3つの風洞(突風、遷音速および超音速風洞)を使用し、風速25m/秒からマッハ数4までの範囲で特性試験を行った。また測定精度は、マッハ数1.5%および流れ角0.4度以内であった。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"NAL enforced high speed characteristic tests of a probe (Pitot tube and body head type) that has carried out research development aiming at an application to Air Data System (ADS) of the SST (Supersonic Transport) and HOPE (H-2 Orbiting Plane). It carried out a characteristic test in Mach number four ranges from wind velocity 25 m/s by using three wind tunnels (gust, transonic and supersonic wind tunnels) of NAL. Also, measurement accuracy was within the Mach number 1.5 percent and flow angle 0.4 degree.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001434013","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"},{"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"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"桑野, 尚明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 正剛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中谷, 輝臣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 弘一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"半沢, 麻雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kuwano, Naoaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Seigo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakaya, Teruomi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hanzawa, Asao","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":"nalsp0038013.pdf","filesize":[{"value":"947.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0038013.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37195/files/nalsp0038013.pdf"},"version_id":"a064b79d-dcd8-4a7f-860a-ecfe84207704"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"高速特性試験","subitem_subject_scheme":"Other"},{"subitem_subject":"プローブ","subitem_subject_scheme":"Other"},{"subitem_subject":"ピトー管","subitem_subject_scheme":"Other"},{"subitem_subject":"4角錐台型5孔プローブ","subitem_subject_scheme":"Other"},{"subitem_subject":"測定精度","subitem_subject_scheme":"Other"},{"subitem_subject":"突風風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"ADS","subitem_subject_scheme":"Other"},{"subitem_subject":"エアデータシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"high speed characteristic test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"probe","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Pitot tube","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multihole pyramidal head probe","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"measurement accuracy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gust wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ADS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Air Data System","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":"四角錐台型5孔プローブを用いた広速度域飛行速度ベクトル計測システムの特性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"四角錐台型5孔プローブを用いた広速度域飛行速度ベクトル計測システムの特性"}]},"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":"37195","relation_version_is_last":true,"title":["四角錐台型5孔プローブを用いた広速度域飛行速度ベクトル計測システムの特性"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:23:41.734692+00:00"}