Calculations of Supersonic Steady Flow

该项目的目的是验证二阶Godunov迎风格式是一种鲁棒、高效、准确和高分辨率的方法，用于涉及复杂非线性波动的三维超音速流场。第一阶段的工作将限于惰性多向气体和简单的几何形状，目的是计算和分析一些模拟斜冲击波反射问题的结果。通过以高度模块化的方式实现该方案，将为第二阶段的工作奠定基础，以便未来的代码开发工作将建立在之前的工作之上。

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.