{"created":"2025-03-21T07:03:43.351524+00:00","id":2000098,"links":{},"metadata":{"_buckets":{"deposit":"a522deaf-de30-4c72-856a-87d70c9f7729"},"_deposit":{"created_by":15,"id":"2000098","owner":"15","owners":[15],"pid":{"revision_id":0,"type":"depid","value":"2000098"},"status":"published"},"_oai":{"id":"oai:cis.repo.nii.ac.jp:02000098","sets":["3:1741764459278"]},"author_link":["699"],"item_10002_biblio_info_7":{"attribute_name":"bibliographic_information","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2025-03-28","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"18","bibliographicNumberOfPages":"9","bibliographicPageEnd":"62","bibliographicPageStart":"54","bibliographic_titles":[{"bibliographic_title":"千葉科学大学紀要","bibliographic_titleLang":"ja"},{"bibliographic_title":"The University Bulletin of Chiba Institute of Science","bibliographic_titleLang":"en"}]}]},"item_10002_description_5":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航空機の主翼周りの流れには，翼端渦と呼ばれる３次元性を持つ強力な縦渦の問題があり，安全上その抑制は大きな課題となっている．また，近年では燃費といった環境面の観点からも翼性能を維持しつつ翼端渦を抑制することが重要となっている．本研究では，３次元数値シミュレーションを用いて，プラズマアクチュエータにより誘起された流れが翼端渦生成に及ぼす影響を解明し，抑制に必要なプラズマアクチュエータの性能を探った.計算結果より，入力電圧に比例して誘起速度が大きくなり，誘起速度の大きさが主流速度を超えると翼端渦の構造に影響を与えることが判明した．また，誘起速度の大きさに比例して翼端渦の抑制効果も高くなり，揚力係数，抗力係数，揚抗比の向上も見られた．本研究により，プラズマアクチュエータを適切な出力で作動させることによって翼端渦が抑制でき，翼性能を向上させることが示された．","subitem_description_language":"ja","subitem_description_type":"Abstract"}]},"item_10002_full_name_3":{"attribute_name":"著者（英）","attribute_value_mlt":[{"names":[{"name":"SATO, Ryoga","nameLang":"en"},{"name":"NAGASE, Aoi","nameLang":"en"},{"name":"TODA, 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