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3 翼型2与翼型S832最大相对厚度、最大相对弯度和升阻比的对比
Table 3 Comparison of maximum relative thickness, maximum relative camber and lift-drag ratio between airfoil 2 and airfoil S832
翼型最大相对厚度/%最大相对弯度/%升阻比ε
S83214.895.1148.049 2
翼型216.317.5846.952 8