@techreport{oai:jaxa.repo.nii.ac.jp:00045089,
 author = {河合, 伸坦 and KAWAI, Nobuhiro},
 month = {Aug},
 note = {In order to analyze inviscid transonic flow around an airfoil, the program has been developed for solving two-dimensional Euler equations by the diagonal form of implicit approximate factorization scheme. Numerical results show two patterns of shocks. One is the flow from supersonic to subsonic, which exhibits nearly normal shock. The other, a flow from supersonic to supersonic, exhibits oblique shock. Numerical solutions of Euler equations are compared with those of potential flow, showing the differences in shock position, and pressure rise after shock., 資料番号: NALTR0831000, レポート番号: NAL TR-831},
 title = {対角化IAF解法による非粘性遷音速流翼型解析},
 year = {1984}
}