词The results show that the unstart boundary of supersonic inlets is mainly concerned with Mach number of freestream without considering the variation of angle of attack.
在不考虑攻角变化的条件下，进气道不起动边界
要与来流马赫数有关。
The results show that the unstart boundary of supersonic inlets is mainly concerned with Mach number of freestream without considering the variation of angle of attack.
在不考虑攻角变化的条件下，进气道不起动边界要与来流马赫数有关。
声明：以上例句、词性
类均由互
网资源自动生
，
未经过人工审核，其表达内容亦不代表本软件的观点；若发现问题，欢迎向我们指正。
