A theory of aeroelastic stability of hingeless rotor blade in hover by using the Galerkin weighted residual finite element method is developed in this paper.
采用伽辽金加权余数有限元素法发展了一种悬停状态下无铰旋气弹稳定性的分析方法。
A theory of aeroelastic stability of hingeless rotor blade in hover by using the Galerkin weighted residual finite element method is developed in this paper.
采用伽辽金加权余数有限元素法发展了一种悬停状态下无铰旋气弹稳定性的分析方法。
声明:以上例句、词性分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。
A theory of aeroelastic stability of hingeless rotor blade in hover by using the Galerkin weighted residual finite element method is developed in this paper.
采用伽辽金加权余数有限元素法展了一种悬停状态下无铰旋翼桨叶气弹稳定性的分析方法。
声明: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,其表达内容亦不代表本软件的观点;若题,欢迎向我们指正。
A theory of aeroelastic stability of hingeless rotor blade in hover by using the Galerkin weighted residual finite element method is developed in this paper.
采用伽辽金加权余数有限元法
展了一种悬停状态下无铰旋翼桨叶气弹稳定性的分析方法。
声明:以上例句、词性分类均由互联网资源自动生成,部分未工审核,其表达内容亦不代表本软件的观点;若
现问题,欢迎向我们指正。
A theory of aeroelastic stability of hingeless rotor blade in hover by using the Galerkin weighted residual finite element method is developed in this paper.
采用伽辽金加权余数有限元素法发展了一种悬停状态下无铰旋翼桨叶气弹稳定性的分析方法。
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,其表达内容亦不代表
软件的观点;若发现问题,欢迎向我们指正。
A theory of aeroelastic stability of hingeless rotor blade in hover by using the Galerkin weighted residual finite element method is developed in this paper.
采用伽辽金加权余数有素法发展了一种悬停状态下无铰旋翼桨叶气弹稳定性的分析方法。
声明: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,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。
A theory of aeroelastic stability of hingeless rotor blade in hover by using the Galerkin weighted residual finite element method is developed in this paper.
采用伽辽金加权余数有限元素法发展了一种悬停状态下无铰旋翼弹稳定性的
析方法。
声明: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。
A theory of aeroelastic stability of hingeless rotor blade in hover by using the Galerkin weighted residual finite element method is developed in this paper.
采用伽辽金加权余数有限元素法发展了一种悬停状态下无铰旋翼桨叶气弹的分析方法。
声明:以上、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。
A theory of aeroelastic stability of hingeless rotor blade in hover by using the Galerkin weighted residual finite element method is developed in this paper.
采用伽辽金加权余数有限元素法发展了一种悬停状态下无铰旋翼桨叶气弹稳定性方法。
声:
例句、词性
类均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
观点;若发现问题,欢迎向我们指正。
A theory of aeroelastic stability of hingeless rotor blade in hover by using the Galerkin weighted residual finite element method is developed in this paper.
采用伽辽金加权余数有限元素法发展了一种悬停状态下无铰旋翼桨叶气弹稳定性的分析方法。
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,其表达内容亦不代表
软件的观点;若发现问题,欢迎向我们指正。