Fuji Heavy Industries Ltd.
Fuji Heavy Industries Ltd.
National Aerospace Laboratory
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory(NAL)
雑誌名
航空宇宙技術研究所特別資料
雑誌名(英)
Special Publication of National Aerospace Laboratory SP-7
巻
7
ページ
107 - 120
発行年
1986-12
抄録（英）
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.
境界要素法プログラムによるナセル干渉の計算
nalsp0007014.pdf
(2.05MB)
