@techreport{oai:jaxa.repo.nii.ac.jp:00043263,
 author = {信太, 良文 and 桑原, 邦郎 and Shida, Yoshifumi and Kuwahara, Kunio},
 month = {Nov},
 note = {Transonic flow around an NACA0012 airfoil at high angle of attack is simulated by solving the two-dimensional Navier-Stokes equations. The block pentadiagonal matrix scheme is employed. Periodic phenomena of shock-wave vortex interaction are observed. For comparison, computation of subsonic flow has been done. Small vortices are observed between the leading edge and the center of the chord., 資料番号: NALSP0008010, レポート番号: NAL SP-8},
 title = {大迎角翼型回りの遷音速流の数値解析},
 year = {1987}
}