Daiko Ltd.
National Aerospace Laboratory
Fujitsu Ltd.
Meitec Ltd.
The Institute of Space and Astronautical Science
Boeing Commercial Airplane Company
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-10
巻
10
ページ
237 - 242
発行年
1989-11
抄録（英）
The viscous transonic flow simulations over B747 wing-fuselage combination were carried out using the three-dimensional Reynolds-averaged thin-layer Navier-Stokes equations. The single grid system in C-O topology is used for these computations, and it has 1.1 million grid-points. Computed results such as total lift and pressure distributions on the wing are in good agreement with the wind tunnel test data.
B747の空力数値シミュレーションと風試によるその精度の検証
nalsp0010040.pdf
(323.4KB)
