{"created":"2023-06-20T15:11:36.282319+00:00","id":41286,"links":{},"metadata":{"_buckets":{"deposit":"cd824735-073c-4e87-8e8c-afe347d927f1"},"_deposit":{"created_by":1,"id":"41286","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41286"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041286","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489248","489250","489249","489253","489251","489246","489247","489252"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Dynamic stability testing at the NAL 2 m Transonic Wind Tunnel. Part 1: Development of model drive apparatus and dynamic balance"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"6","bibliographicPageStart":"1","bibliographicVolumeNumber":"45","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_3_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":"20-21 May 1999 (62nd). 25-26 Nov. 1999 (63rd)","subitem_description_type":"Other"}]},"item_3_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":"20-21 May 1999 (62nd). 25-26 Nov. 1999 (63rd)","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"NALの2m遷音速風洞におけるHOPE-X(宇宙往還技術試験機)の動安定変数を測定するために、強制加振法を用いる新しいタイプのピッチあるいはヨー、およびロールの試験装置と動的天秤を開発した。カムを用いたドライブ装置は軸方向に比較的短くしてあるが、装置は遷音速域で使用するために高負荷と高い加振周波数に耐えねばならなかった。動的天秤は高剛性ビームを有するので、高レベル出力信号を得るために動的天秤内にプリアンプを内蔵した。装置の性能を確認するために、新しいデータ整理技術を用いて、風袋条件における動的安定変数を同定する試験を行った。ダミー模型のモーメントI(sub X)およびI(sub Y)を測定した結果、ピッチあるいはヨー、およびロール天秤システムは良好な性能を示した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"To measure dynamic stability parameters of HOPE-X (H-2 Orbiting Plane-Experimental) at the NAL 2 m Transonic Wind Tunnel, new types of pitch/yaw and roll model drive apparatus and dynamic balance for forced oscillation techniques are developed. The drive apparatus applied cams are relatively longitudinally short, though they have to endure high load and high drive frequencies for the transonic region use. Pre-amplifier in the balance is utilized to get high level output signals because the dynamic balance has beams with high stiffness. For the verification of performance of the apparatus, testing was conducted with the use of new data reduction technique to identify the dynamic stability parameters at the condition of tare. Measurement of moments I(sub X) and I(sub Y) of a dummy model indicated good performance of the pitch/yaw and roll balance systems.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028634001","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 SP-45","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":"0289-260X","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":"AN10097345","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"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"川崎重工業"},{"subitem_text_value":"川崎重工業"}]},"item_3_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":"Kawasaki Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"三輪, 等"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"上野, 真"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"米本, 浩一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"志子田, 繁一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miwa, Hitoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueno, Makoto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yonemoto, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shikoda, Shigeichi","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":"nalsp0045001.pdf","filesize":[{"value":"2.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0045001.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41286/files/nalsp0045001.pdf"},"version_id":"987f4ec5-d30f-46bc-9534-89466dfeb6aa"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"動安定試験","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE-X","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"ピッチ・ヨー・ロール天秤システム","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速","subitem_subject_scheme":"Other"},{"subitem_subject":"模型加振装置","subitem_subject_scheme":"Other"},{"subitem_subject":"動的天秤","subitem_subject_scheme":"Other"},{"subitem_subject":"強制加振法","subitem_subject_scheme":"Other"},{"subitem_subject":"動安定微係数","subitem_subject_scheme":"Other"},{"subitem_subject":"データ整理","subitem_subject_scheme":"Other"},{"subitem_subject":"性能評価","subitem_subject_scheme":"Other"},{"subitem_subject":"カム","subitem_subject_scheme":"Other"},{"subitem_subject":"モーメント","subitem_subject_scheme":"Other"},{"subitem_subject":"風袋","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙往還技術試験機","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic stability testing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE X","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel testing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pitch yaw roll balance system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model drive apparatus","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic balance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"forced oscillation technique","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic stability parameter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"data reduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"performance evaluation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cam","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"moment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"tare","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane Experimental","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":"遷音速動安定試験　その1:試験装置と動的天秤の開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"遷音速動安定試験　その1:試験装置と動的天秤の開発"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41286","relation_version_is_last":true,"title":["遷音速動安定試験　その1:試験装置と動的天秤の開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:03:59.843901+00:00"}