Kawasaki Heavy Industries Co. 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
39 - 44
発行年
1986-12
抄録（英）
A numerical investigation of wing/nacelle interferences of USB configuration was carried out. A grid system about the realistic configuration of wing/nacelle combination was generated by the multi-block grid generation technique. The Euler equations were solved by the second order accurate upwind scheme. Results were obtained for M infinity = 0.7, alpha = 2.0. The existence of channel flows accompanied by strong shocks between two engine nacelles were confirmed. Power effects of two engines were examined by modeling both the plane of intake and that of jet exhaust appropriately.
オイラー方程式による翼ナセル干渉解析
nalsp0007005.pdf
(446.65KB)
