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。
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。
声明:、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,进气
动边界主要与来流马赫数有关。
声明:以上句、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
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。
声明:以上句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表
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.
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。
声明: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
达内容亦不代
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:
、词
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。
声明:以上句、词性分类均由互联网资源自动生成,部分未经过人工
,
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下,进气道不起动边界主要与来流马赫数有关。
声明:以上句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现
,
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。
声明:以上句、词性分类均由互联
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件
,进气道不起动边界主要与来流马赫数有关。
声明:以上句、词性分类均由互联网资源自动生成,部分未经过人
,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。