並列タイトル等Computation of Nacelle Interference Using Boundary Element Method
タイトル(掲載誌)航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-7
一般注記The aerodynamic interference problem of jet transport aircraft due to the close coupling between nacelle and wing is one of the major concerns of aerodynamic engineers. At the research level, the Navier-Stokes code is beginning to be applied to such a problem. At the engineering level the application of the panel method is more practical. This paper presents the results of applying the Boundary Element Method (a new generation panel method developed by the National Aerospace Laboratory) code to the analysis of nacelle interference of a practical jet transport configuration. Correlation between calculated and tested results is also presented.
資料番号: NALSP0007014
レポート番号: NAL SP-7
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ