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aerodynamics's Introduction

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: $12%$

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