Using axisymmetric full Navier-Stokes equations, the thermo-chemical nonequilibrium flow in hypersonic nozzle was simulated and the scale effects due to nonequilibrium were analysed numerically.
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释义
摘要采用轴对称热化学非平衡全N-S方程,数值分析了高超声速喷管流场中非平衡引起的尺度效应。
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