Solution of Pressure Coefficient for flow around Cyliner without Lift by GSL in C/C++ Toolkit chains Visual Studio vcpkg gsl matplotlibcpp Anaconda (Python with matplotlib and numpy) Algorithm Specification NACA_23012 设计升力系数: $2 \times 0.15 = 0.3$ 最大弯度位置和弦长之比百分数: $30 \div 2 = 15%$ 最大厚度与弦长之比百分数: $12%$