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三次元亜音速非定常空気力のラプラス領域での数値計算
https://jaxa.repo.nii.ac.jp/records/43219
https://jaxa.repo.nii.ac.jp/records/432196f5bb069-a72b-4aca-89ed-971788773faf
名前 / ファイル | ライセンス | アクション |
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nalsp0007003.pdf (539.0 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 | 三次元亜音速非定常空気力のラプラス領域での数値計算 | |||||
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 | Numerical Calculation in the Laplace Domain for Subsonic Unsteady Aerodynamic Forces Acting on a Finite Wing | |||||
著者 |
上田, 哲彦
× 上田, 哲彦× Ueda, Tetsuhiko |
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著者所属 | ||||||
航空宇宙技術研究所機体第一部 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
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特別資料 en : Special Publication of National Aerospace Laboratory SP-7 巻 7, p. 25-32, 発行日 1986-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A method of obtaning subsonic unsteady aerodynamic forces in the Laplace domain is presented in this paper. The kernel function of singular integral equations based on the lifting surface theory is numerically computed in the exact way for the entire s-plane. In an example calculation of the generalized forces, a singularity appears in the left half of the p-plane at a high Mach number of eight-tenths. It is shown that the singularity is a pole of the order one and that it can be modeled by a simple rational function which is relevant to the aeroelastic analysis. The theory of functions is utilized for obtaining the singularity model for the generalized forces. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALSP0007003 | |||||
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 SP-7 |