FEM FCT is used to solve three dimensional hypersonic inviscid flow. 从Euler方程出发，利用流量修正有限元法（FEM?FCT）求解三维无粘流动的高速流场。
Hypersonic propulsion test facility is important for the scramjet ground tests. 摘要高超声速推进风洞是进行超燃冲压发动机模型地面模拟的重要试验设备。
A conceptual design of the hypersonic civil transport is introduced here. 介绍了高超声速民用运输机的概念设计方案。
Hypersonic wind tunnels operating at very low densities were developed starting in about 1960. 低密度超音速风洞大约开始发展于1960年。
Departures form the ideal practice followed by the Wright have been particularly noticeable in the development of supersonic and hypersonic vehicles. 特别值得注意的是在发展超音速和高超音速飞行器的过程中，偏离了莱特理想的工作方式。
With such a large heat sink value, FRA can meet the requirement of hypersonic flying machine. 在 80 0℃时 ,两者都具有较高的热沉值 ,分别达到 5 6 9MJ kg和 6 6 0MJ kg ,该热沉值能够满足超高音速飞行器的热管理要求。
