基于数论网格法与Morris法的翼型气动特性敏感性分析
文泽军,孟祥恒,肖钊,张帆

Sensitivity analysis of airfoil aerodynamic characteristics based on NT-net method and Morris method
Ze-jun WEN,Xiang-heng MENG,Zhao XIAO,Fan ZHANG
表2 翼型1与翼型S832前缘半径和升阻比的对比
Table 2 Comparison of leading edge radius and lift-drag ratio between airfoil 1 and airfoil S832
翼型前缘半径/mmε
S8320.7048.049 2
翼型10.7548.708 3