@techreport{oai:jaxa.repo.nii.ac.jp:00045305,
 author = {福田, 正大 and 廣瀬, 直樹 and 河合, 伸坦 and 中橋, 和博 and 菊野, 栄次 and FUKUDA, Masahiro and HIROSE, Naoki and KAWAI, Nobuhiro and NAKAHASHI, Kazuhiro and KIKUNO, Eiji},
 month = {Dec},
 note = {The two-dimensional Navier-Stokes codes, NSFOIL and NS2D, are validated in terms of analysis of practical thin-airfoils for conventional propeller systems and compared with data obtained from wind-tunnel tests. This research was done as part of an aerodynamic research project on propeller blades for advanced turboprop (ATP) engines. The comparison was made at a Reynolds number of 8 million which was equivalent to the actual flight condition of ATP, and it was shown that these codes provide very effective tools for predicting nonlinear characteristics of thin-airfoils. In the course of careful comparison, some improvements on these codes were clarified., 資料番号: NALTR1046000, レポート番号: NAL TR-1046},
 title = {Investigation of ATP blades (Part II)-Validation of Two-dimensional Viscous Flow Simulation Codes around Thin Airfoils-},
 year = {1989}
}