... hypersonic range 特超声速区hypersonic region特超声速区 hypersonic shock tube 高超声速激波管 ...
双语例句
1
The results show that the shock wave structure is unsteady in shock induced hypersonic turbulent separated flows, generating an intermittent region.
结果表明:在激波诱导的高超音速湍流分离流中,激波结构是不稳定的,产生一个间歇区域。
2
In this paper, the nonequilibrium viscous shock layer equations have been used to calculate the hypersonic flows over blunt bodies in the fore-body region (including stagnation line and sonic line).