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,进气道不起动边界来流马赫数有关。
声:以上例句、词性分类
联网资源自动生成,部分未经过人工审核,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。
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,进气道不起动边界主要与来流马赫数有关。
声:以上
、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达
不代表本软件的观点;若发现问题,欢迎向我们指正。
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.
在不考虑化的条件下,进气道不起动边界主要与来流马赫数有关。
声:以上例句、词性分类均由互联网资源自动生成,部分未经过
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。
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.
在考虑攻角变化的条件下,进
起
边界主要与来流马赫数有关。
声:以上例句、词性分类均由互联网资源
成,部分未经过人工审核,其表达内容亦
代表本软件的观点;若发现问题,欢迎向我们指正。
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,进气道不起动边界主要马赫数有关。
声:以上例句、词性
由互联网资源自动生成,部
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。
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.
在不考虑攻角变化件下,进气道不起动边界主要与来流马赫数有关。
声:以上例句、词性
类均由互联网资源自动生成,部
过人工审核,其表达内容亦不代表本软件
观点;若发现问题,欢迎向我们指正。
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.
在不考虑攻角变化条件下,进气道不起动边界主要与来流马赫数有关。
声:以上例句、词性分类均由互联网资源自动生成,部分
经过人工审核,其表达内容亦不代表本软件
观点;若发现问题,欢迎向我们指正。
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,
气道不起动边界主要与来流马赫数有关。
声:以上例句、词性
类均由互联网资源自动生
,
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。
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.
考虑攻角变化的条件下,进气道
起动边界主要与来流马赫数有关。
声:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其
容亦
代
本软件的观点;若发现问题,欢迎向我们指正。