@techreport{oai:jaxa.repo.nii.ac.jp:00043369,
 author = {伊藤, 良三 and 佐藤, 求 and 高梨, 進 and 藤井, 孝蔵 and 松島, 紀佐 and Ito, Ryozo and Sato, Motomu and Takanashi, Susumu and Fujii, Kozo and Matsushima, Kisa},
 month = {Nov},
 note = {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., 資料番号: NALSP0010040, レポート番号: NAL SP-10},
 title = {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},
 year = {1989}
}