{"created":"2023-06-20T15:07:27.189420+00:00","id":36826,"links":{},"metadata":{"_buckets":{"deposit":"3c8cd920-e937-4406-bc23-9b660ae7c132"},"_deposit":{"created_by":1,"id":"36826","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36826"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036826","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["425051","425052"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"3次元圧縮流における境界層遷移の予測法"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"51","bibliographicPageStart":"39","bibliographicVolumeNumber":"31","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_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"超音速翼上の境界層の遷移位置を予測するための効率的な数値計算法を提案した。この計算システムは3次元境界層、その線形安定性およびN因子の計算から構成されている。3種類の計算の各々は大量の計算時間と各計算間の複雑な干渉手続きを必要とする。従って、計算時間を節約し計算システムをできるだけ簡素なものにするために、境界層の計算と線形安定性の計算に対して同じ計算アルゴリズムを用いた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An efficient numerical calculation method for predicting the transition location of the boundary layer over a supersonic wing was proposed. This numerical system consists of the calculations of Three Dimensional (3-D) boundary layer, its linear stability characteristics, and N factor. Each of the three calculations requires a lot of computing time and a rather complex interference procedure between each calculation. Therefore, the same computing algorithm for both boundary layer and linear stability calculations was used to save computing time and to make the calculation system as simple as possible.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000440003","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-31","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 空力性能部"}]},"item_5_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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"石田, 洋治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishida, Yoji","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":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0031003.pdf","filesize":[{"value":"768.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0031003.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36826/files/nalsp0031003.pdf"},"version_id":"875f437f-3559-4c82-84bc-50cf841d08e6"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"3次元圧縮流","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層遷移","subitem_subject_scheme":"Other"},{"subitem_subject":"遷移位置予測法","subitem_subject_scheme":"Other"},{"subitem_subject":"計算アルゴリズム","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速翼","subitem_subject_scheme":"Other"},{"subitem_subject":"数値計算法","subitem_subject_scheme":"Other"},{"subitem_subject":"線形安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"N因子","subitem_subject_scheme":"Other"},{"subitem_subject":"計算時間","subitem_subject_scheme":"Other"},{"subitem_subject":"three dimensional compressible flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer transition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transition location prediction method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"calculation algorithm","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical calculation method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"linear stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"N factor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"calculation time","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Prediction method of boundary layer transition in 3-D compressible flow","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Prediction method of boundary layer transition in 3-D compressible flow","subitem_title_language":"en"}]},"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":"36826","relation_version_is_last":true,"title":["Prediction method of boundary layer transition in 3-D compressible flow"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:49:44.040389+00:00"}