{"created":"2023-06-20T15:08:17.603006+00:00","id":37705,"links":{},"metadata":{"_buckets":{"deposit":"5749a4dc-6634-4587-a64f-0c196ce6f0cf"},"_deposit":{"created_by":1,"id":"37705","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37705"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037705","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482593","482592"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical solution of inverse problem in aerodynamics"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"108","bibliographicPageStart":"105","bibliographicVolumeNumber":"19","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第10回航空機計算空気力学シンポジウム論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of the NAL symposium on aircraft computational aerodynamics","bibliographic_titleLang":"en"}]}]},"item_5_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":"航空宇宙技術研究所 10-12 Jun. 1992 東京 日本","subitem_description_type":"Other"}]},"item_5_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":"National Aerospace Laboratory 10-12 Jun. 1992 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"空気力学における最も重要な逆問題の1つとして、定まった平面形の翼につき望ましい表面圧力分布が与えられた場合の翼断面形を見出す問題がある。この問題は、遷音速積分方程式に基づいた「残差修正」法により解くことができる。本論文では、ナビエ・ストークス方程式を含む種々の流れ解法と組み合せた積分方程式法の最近の適用例のいくつかを示す。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"One of the most important inverse problems in aerodynamics is defined as the problem of finding the wing section contour given the desired surface pressure distribution for a fixed wing planform. This problem can be solved by the 'residual-correction' method based on the transonic integral equations. In this paper, some of the recent applications of the integral equation method using various analysis codes including Navier-Stokes codes is presented.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004168019","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-19","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"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"高梨, 進"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takanashi, Susumu","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":"nalsp0019019.pdf","filesize":[{"value":"303.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0019019.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37705/files/nalsp0019019.pdf"},"version_id":"52ab24f1-d467-46b6-83e6-06911d9d6134"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"空力設計主翼","subitem_subject_scheme":"Other"},{"subitem_subject":"翼断面","subitem_subject_scheme":"Other"},{"subitem_subject":"スーパークリティカル翼","subitem_subject_scheme":"Other"},{"subitem_subject":"層流翼","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速翼","subitem_subject_scheme":"Other"},{"subitem_subject":"逆問題解法","subitem_subject_scheme":"Other"},{"subitem_subject":"繰返し手法設計解法","subitem_subject_scheme":"Other"},{"subitem_subject":"残差修正法","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速積分方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"空力最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD解析","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学解析","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing section","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supercritical airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laminar flow airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inverse problem solution procedure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"iterative design procedure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"residual correction method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic integral equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing","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 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