{"created":"2023-06-20T14:36:13.629124+00:00","id":2539,"links":{},"metadata":{"_buckets":{"deposit":"42d522eb-db2b-420a-ba3b-cc9162aec607"},"_deposit":{"created_by":1,"id":"2539","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2539"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002539","sets":["1887:1893","9:1090:1186:1194"]},"author_link":["7102","7097","7101","7100","7104","7098","7099","7103"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Surface Pressure Measurement on Axisymmetric Bodies in Supersonic Flow"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2012-03-09","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"21","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RM-11-016","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料"},{"bibliographic_title":"JAXA Research and Development Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"超音速流中におかれた軸対称物体上に発達する境界層流れに対する遷移機構の理解を促進するとともに，数値流体解析の結果を検証することを目的として，軸対称物体の表面静圧分布計測を宇宙航空研究開発機構が所有する1m×1m超音速風洞において実施した．その結果，従来の静圧孔を用いた表面静圧分布の計測結果は，全面層流を仮定した数値流体解析結果と計測の不確かさの範囲内でよく一致していることが確認された．表面静圧は風洞測定部内の自由流マッハ数分布の影響を受けることがわかったが，その影響は境界層遷移に対しては無視できることが確認された．","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Surface pressure measurement on axisymmetric bodies in supersonic flow was performed in 1m×1m supersonic wind tunnel in Japan Aerospace Exploration Agency, for the purposes of promoting understanding of transition mechanism, and of validation of computational fluid dynamics, for boundary layers on axisymmetric bodies in supersonic flow. It is confirmed that results of surface pressure measurement by use of conventional pressure tap were in good agreement with numerical results of computational fluid dynamics within the range of the assured measurement precision. Moreover, it is found that the pressure distribution is affected by non-uniformity of freestream in the test section of the wind tunnel, but the influence is negligible small for transition prediction.","subitem_description_type":"Other"}]},"item_3_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_3_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0065214000","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: JAXA-RM-11-016","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1121","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":"AA11983593","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構航空プログラムグループ超音速機チーム (JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部風洞技術開発センター計算科学研究グループ"},{"subitem_text_value":"三向ソフトウェア開発"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部風洞技術開発センター計算科学研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Supersonic Transport Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Wind Tunnel Technology Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Sanko Soft"},{"subitem_text_language":"en","subitem_text_value":"Wind Tunnel Technology Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"徳川, 直子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"赤塚, 純一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石川, 敬掲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中北, 和之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tokugawa, Naoko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Akatsuka, Junichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishikawa, Hiroaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakakita, Kazuyuki","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":"2020-01-15"}],"displaytype":"detail","filename":"65214000.pdf","filesize":[{"value":"2.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"65214000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2539/files/65214000.pdf"},"version_id":"1c375c1e-9836-4852-824c-3ad5d3604979"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"pressure measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"axisymmetric bodies","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flow","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":"超音速流中に置かれた軸対称物体の表面静圧分布計測","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速流中に置かれた軸対称物体の表面静圧分布計測"}]},"item_type_id":"3","owner":"1","path":["1194","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2539","relation_version_is_last":true,"title":["超音速流中に置かれた軸対称物体の表面静圧分布計測"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:20:30.143802+00:00"}