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.

• 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。