@techreport{oai:jaxa.repo.nii.ac.jp:00043170,
 author = {河合, 伸坦 and 廣瀬, 直喜 and Kawai, Nobuhiro and Hirose, Naoki},
 month = {Nov},
 note = {High Reynolds number transonic flow around an airfoil is numerically analyzed. The implicit approximate factorization scheme is used for the Navier-Stokes equations with an algebraic eddy viscosity model of the turbulent boundary layer. The boundary conditions on the airfoil and along the wake cut are implicitly handled. Computed results of short bubble and shock-induced separation are demonstrated. Inviscid transonic flow around an airfoil is also numerically analyzed. The diagonal form of the implicit approximate factorization scheme is used for computational efficiency. Some of the results are compared with those of potential flow calculations., 資料番号: NALSP0003028, レポート番号: NAL SP-3},
 title = {高レイノルズ数遷音速流翼型解析},
 year = {1984}
}