hypersonic nozzle meaning in Chinese

高超音速喷管

The design and computation of the hypersonic nozzle have scientific and practical value to solve these problems
而高超声速风洞喷管的设计和计算则对解决这一类问题具有重要的科学意义和实用价值。
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。
The results show that to design a supersonic / hypersonic nozzle of wind tunnel must consider the effect of variable specific heat , which gives reference to nozzle and wind tunnel design
考虑这一因素后，喷管出口马赫数接近设计马赫数，其设计精度有较大提高。本方法可为超音速高超声速喷管设计和反设计提供参考。