@techreport{oai:jaxa.repo.nii.ac.jp:00043221,
 author = {沢田, 恵介 and 高梨, 進 and Sawada, Keisuke and Takanashi, Susumu},
 month = {Dec},
 note = {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., 資料番号: NALSP0007005, レポート番号: NAL SP-7},
 title = {オイラー方程式による翼ナセル干渉解析},
 year = {1986}
}