Calculations of Supersonic Steady Flow

本项目的目标是验证第二个- 阶Goddom迎风格式是一种鲁棒、高效、精确、 三维超声速流场高分辨方法 涉及复杂的非线性波动。 第一阶段的工作将是 限于惰性多变气体和简单的几何形状， 目的是计算和分析几种情况下的结果， 模拟斜激波反射问题。 基础设施将 为第二期工程奠定基础， 模块化的方式，使未来的代码开发工作将建立 之前的工作。

The objective of this project is to verify that the second- order Godunov upwind scheme is a robust, efficient, accurate, and high-resolution methodology for 3D supersonic flowfields involving complex nonlinear wave motion. Phase I work will be limited to inert polytropic gases and simple geometries, with the goal to calculate and analyze the results for a few cases of the analogue oblique shock-wave reflection problem. Groundwork will be laid for Phase II work by implementing the scheme in a highly modular fashion, so that future code development work will build on preceding work.