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FA-200改機の動安定微係数
https://jaxa.repo.nii.ac.jp/records/43757
https://jaxa.repo.nii.ac.jp/records/437576152ea1c-d742-4064-b6f7-bed3ef4e29e8
名前 / ファイル | ライセンス | アクション |
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naltm00173.pdf (921.4 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | FA-200改機の動安定微係数 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Dynamic Stability Derivatives of A Modified FA-200 Airplane | |||||
著者 |
遠藤, 浩
× 遠藤, 浩× 林, 良生× 海老沼, 幸成× 中谷, 輝臣× ENDO, Hiroshi× HAYASHI, Yoshio× EBINUMA, Yukinari× NAKAYA, Teruomi |
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著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所資料 en : Technical Memorandum of National Aerospace Laboratory 巻 173, p. 12, 発行日 1970-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The low-subsonic rotary dynamic derivatives of a conventional type of airplane, FA-200 modified, were measured by means of the forced-oscillation apparatus in the NAL 6m low- speed wind-tunnel. The results were compared with the theoretical values calculated by the standard estimation formulae worked out by various authors. It is shown that the calculated values are in fairly good agreement with the measured ones, except when the separation of air-flow is supplsed to occur on the wings in course of the pitching oscillation. The accuracy of measurement of Cnr was rather low, presumably becacuse the vertical tail moved, crossing the unsteady wake behind the fuselage, in yawing oscillation. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0452-2982 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00314334 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTM0173000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TM-173 |