@techreport{oai:jaxa.repo.nii.ac.jp:00043177,
 author = {小松, 浩司 and 飯田, 栄治 and 河村, 龍馬 and 廣瀬, 直喜 and 松野, 謙一 and Komatsu, Koji and Iida, Eiji and Kawamura, Ryuma and Hirose, Naoki and Matsuno, Ken-ichi},
 month = {Nov},
 note = {A comparison of the result of numerical analysis with experimental data is made for the ONERA M-6 and the practical transonic wing model 720211. The Jameson-Caughey's transonic wing programs FLO22 and FLO27 are used. The wing aerodynamic characteristics with viscous effect are evaluated by taking into account the boundary layer friction drag. This drag is calculated by using a three-dimensional compressible boundary layer program for wings, BLAY. Finally, a viscous-inviscid interaction procedure for FLO27-BLAY is proposed, and a preliminary result is presented., 資料番号: NALSP0003035, レポート番号: NAL SP-3},
 title = {遷音速後退翼に対する境界層効果の評価},
 year = {1984}
}