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.
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。
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.
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,其达内容亦不
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.
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,其达内容亦不
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.
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,其达内容亦
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一种悬停状态下无铰旋翼桨叶气弹稳定性的
析方法。
声明: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。