{"created":"2023-06-20T15:10:13.329943+00:00","id":39816,"links":{},"metadata":{"_buckets":{"deposit":"6939d887-5bbc-4f99-bfd7-c9ccc141f4dc"},"_deposit":{"created_by":1,"id":"39816","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39816"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039816","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["444625","444635","444629","444632","444630","444626","444627","444634","444628","444624","444631","444633"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The first estimations of wind tunnel uncertainties for HOPE"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"12","bibliographicPageStart":"1","bibliographicVolumeNumber":"704","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航技研と宇宙開発事業団は無人有翼往還機(HOPE)の開発研究を研究共同チームを組んで進めている。HOPEの風試誤差を設定する第一歩として同一HOPE2.5％縮尺模型、天秤、スティングを用いて、航技研2m×2m遷音速風洞と川崎重工業(株)1m×1m遷音速風洞による対応風洞試験を実施した。風試誤差を同じマッハ数、一定迎角における両風洞試験結果の差を集めたデータ群の自乗平均平方根として求め、天秤計測誤差と比較した。風試誤差はマッハ数1付近を除いた速度域では、天秤精度と同程度かそれ以下であった。また最後に、類似形状模型による風洞試験データが風試誤差設定に使用可能であることを示唆した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The H-2 Orbiting Plane (HOPE) launched by an H-2 rocket or its derivative, is being studied by the NAL and the NASDA. Wind tunnel tests were performed using the same HOPE 2.5 percent scale model using the same balance and sting as the first step in developing wind tunnel uncertainties for HOPE. NAL 2 m x 2 m transonic wind tunnel and KHI 1 m x 1 m transonic wind tunnel which belongs to Kawasaki Heavy Industries Ltd., were used in the transonic speed range. Wind tunnel uncertainties which are estimated as root mean square values calculated from differences between two wind tunnel test results, are called tolerances in this report. Tolerances are compared with force measurement accuracy of the sting type balance and turn out to be almost the same order of balance error except in the about Mach number one speed range. Finally it is shown that wind tunnel test data with a model, the configuration of which is similar to HOPE, can be available in developing tolerances for HOPE, from comparison of tolerances between present wind tunnel test data and the past HOPE series wind tunnel test data.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000679000","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 TM-704","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":"0452-2982","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":"AN00314334","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 空力性能部"},{"subitem_text_value":"航空宇宙技術研究所 空力性能部"},{"subitem_text_value":"航空宇宙技術研究所 空力性能部"},{"subitem_text_value":"航空宇宙技術研究所 空力性能部"},{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"宇宙開発事業団"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"青木, 武夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 弘一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"細江, 信幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 正剛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松田, 昌三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高野, 純"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aoki, Takeo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hosoe, Nobuyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Seigo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuda, Masami","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takano, Jun","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":"2020-01-27"}],"displaytype":"detail","filename":"naltm00704.pdf","filesize":[{"value":"1.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00704.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39816/files/naltm00704.pdf"},"version_id":"8960fe8b-078a-4280-b578-5fd9124402ca"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2ロケット打上げ型有翼回収機","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙船","subitem_subject_scheme":"Other"},{"subitem_subject":"風試誤差","subitem_subject_scheme":"Other"},{"subitem_subject":"風試公差","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"スティング型天秤","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 orbiting plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel uncertainty","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"tolerance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sting type balance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","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":"HOPE風試誤差の初期評価","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HOPE風試誤差の初期評価"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39816","relation_version_is_last":true,"title":["HOPE風試誤差の初期評価"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:18:50.514371+00:00"}