Meshless MUSCL scheme, which resolves shock tube problems well and is easy to extend to higher dimensions.
无网格的MUSCL格式，这种方式能够较好的模拟激波问题，并且易于推广到高维。
In this paper, the numerical results of burning gas flow in the vertical launch system of a rocket are reported. A second-order accurate MUSCL scheme is employed.
本文报导了火箭垂直发射系统燃气流场的数值计算结果，在计算中采用二阶精度的MUSCL格式。
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