{"created":"2023-06-20T14:39:25.822143+00:00","id":6177,"links":{},"metadata":{"_buckets":{"deposit":"ae608250-06c1-4c56-9e01-95d39597cf0a"},"_deposit":{"created_by":1,"id":"6177","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6177"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006177","sets":["1887:1891","9:789:1031:1053"]},"author_link":["30956","30946","30954","30948","30945","30949","30953","30947","30952","30951","30950","30955"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Stereoscopic PIV system applied to JAXA 2 m x 2 m Transonic Wind Tunnel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-02-28","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"41","bibliographicPageStart":"34","bibliographicVolumeNumber":"JAXA-SP-05-016","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第74回風洞研究会議論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 74th Meeting","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"これまで主に低速風洞において整備を進めてきた可搬型PIVシステムに対して、遷音速風洞での適用を目的とした改良を加えた遷音速風洞用ステレオPIVシステムの開発を行った。計測システムの開発では、遷音速風洞において実用化を困難としている、プレナム室による制約、シード投入方法ならびにセッティング時間の制約に対して、PIV機器の遠隔操作システムを構築し、遷音速風洞でのPIV計測を可能とするための改良を行った。開発された計測システムを用い、JAXA2m×2m遷音速風洞(TWT1)におけるステレオPIV計測の実用化を目的とした予備試験を実施した。予備試験では、遷音速風洞における計測可能性の確認および技術的問題点の把握に必要なデータを取得した。試験はSSTジェット実験機圧力模型を対象とし、フロースルーナセル周りの流れを中心に計測を行った。PIV計測結果は、シュリーレン可視化画像ともよく一致し、TWT1におけるステレオPIV計測の妥当性が示された。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Stereoscopic PIV technique was applied to the JAXA next-generation supersonic transport (SST) jet experimental airplane model. The measurements have been performed in the JAXA 2 m x 2 m Transonic Wind Tunnel. Application of PIV measurement techniques to transonic wind tunnels has particular difficulties associated with complex flows with shock waves. Due to these difficulties, practical experiments of PIV measurements in transonic wind tunnels are limited. In the present study, a fully remote-controlled stereoscopic PIV system is developed for velocity measurement of transonic complex flows, and preliminary results using the system are reported to evaluate the system capabilities. The tests were conducted at a freestream Mach number from 0.4 to 1.4. An example of raw PIV images was captured by the camera around the flow-through nacelle intake. Location and shape of shock waves observed in the PIV results are in good agreement with schlieren results for identical test condition. The velocity field information of the PIV results is valuable in a precise validation of CFD.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049211006","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: JAXA-SP-05-016","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"IHIエアロスペース・エンジニアリング"},{"subitem_text_value":"コスモテック"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"IHI Aerospace Engineering Co. Ltd."},{"subitem_text_language":"en","subitem_text_value":"Cosmotec Co. Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"加藤, 裕之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡辺, 重哉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"唐沢, 敏夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野口, 正芳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋本, 拓郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉村, 定修"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kato, Hiroyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Shigeya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Karasawa, Toshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noguchi, Masayoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashimoto, Takuro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshimura, Sadanori","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":"2020-01-16"}],"displaytype":"detail","filename":"49211006.pdf","filesize":[{"value":"2.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49211006.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6177/files/49211006.pdf"},"version_id":"06b04956-3575-4dd4-a747-0106e825268a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"粒子画像流速測定法","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"立体視","subitem_subject_scheme":"Other"},{"subitem_subject":"ステレオPIVシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"流速","subitem_subject_scheme":"Other"},{"subitem_subject":"速度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"YAGレーザ","subitem_subject_scheme":"Other"},{"subitem_subject":"CCDカメラ","subitem_subject_scheme":"Other"},{"subitem_subject":"シーディング法","subitem_subject_scheme":"Other"},{"subitem_subject":"シャイムフラグ条件","subitem_subject_scheme":"Other"},{"subitem_subject":"速度ベクトル","subitem_subject_scheme":"Other"},{"subitem_subject":"particle image velocimetry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stereoscopic vision","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stereoscopic PIV system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow velocity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"velocity distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"YAG laser","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CCD camera","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"seeding method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Scheimflug condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"velocity vector","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":"可搬型PIVシステムの遷音速風洞への適用","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"可搬型PIVシステムの遷音速風洞への適用"}]},"item_type_id":"5","owner":"1","path":["1053","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6177","relation_version_is_last":true,"title":["可搬型PIVシステムの遷音速風洞への適用"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:00:44.092074+00:00"}