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航空機開発における計算空気力学
https://jaxa.repo.nii.ac.jp/records/43129
https://jaxa.repo.nii.ac.jp/records/43129fa97133d-e783-42ce-a583-cac6c412bb5d
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
nalsp0001011.pdf (660.3 kB)
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| Item type | テクニカルレポート / Technical Report(1) | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| 公開日 | 2015-03-26 | |||||||||
| タイトル | ||||||||||
| タイトル | 航空機開発における計算空気力学 | |||||||||
| 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 | Computational Aerodynamics in Designing Aircraft | |||||||||
| 著者 |
河野, 通陽
× 河野, 通陽
× Kono, Michi-aki
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| 著者所属 | ||||||||||
| 三菱重工業株式会社 | ||||||||||
| 著者所属（英） | ||||||||||
| en | ||||||||||
| Mitsubishi Heavy Industries Co.Ltd. | ||||||||||
| 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-1 巻 1, p. 91-100, 発行日 1983-11 |
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| 抄録（英） | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | A historical review of how computational aerodynamics has been utilized in the major aircraft developments in our company is given in this paper. The following is the representative aerodynamic calculation technology used in each aircraft. (1) MU-2 business turbo-prop airplane A pair of sources are introduced to simulate the airflow past the spoiler which is the aerodynamic feature of the aircraft. (2) XC-1 The potential flow theory with boundary layer correction is used for wing design together with the panel method for air-intakes. (3) XT-2 The transonic and supersonic area-rule was a reliable guide in the design of the fuselage, and the lifting surface theory was effective in the design of a wing with a small aspect ratio. (4) MU-300 business jet airplane Transonic aerodynamic calculations were ready for use, such as the transonic full potential code for airfoils and the small disturbance code for wings. It is more important than ever before to keep up with the world's leading technology aerodynamics, since it will play a more dominant role in aircraft development. Especially it is strongly hoped that viscous effects can be evaluated with reasonable accuracy. As far as our computing machines are concerned, fortunately, first class machines have been available, whereas a super computer for large scale calculation will certainly be beyond one company's capability. In summary, both software and hardware must be developed by the joint efforts of private enterprise and the government in order for Japan to become a leader of world technology in the future. | |||||||||
| 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: NALSP0001011 | |||||||||
| 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-1 | |||||||||
