In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
在气动弹性领域中,人们在设计过程中最为是颤振现象。
In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
在气动弹性领域中,人们在设计过程中最为是颤振现象。
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了一种悬停状态下无铰旋翼桨叶气弹稳定性
法。
声明:以上例句、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。
In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
在气动弹性领域中,人们在设计过程中最为是颤振现象。
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了一种悬停状态下无铰旋翼桨叶气弹稳定性
法。
声明:以上例句、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。
In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
在气动弹性领域中,人们在程中最为关心的是颤振现象。
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、词性分类均由互联网资源自动生成,部分未经
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。
In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
在气动弹性领域中,人们在设计过程中最为关心的是颤振现象。
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,
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。
In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
在气动弹性领域中,人们在设中最为关心的是颤振现象。
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:句、词性分类均由互联网资源自动生成,部分未经
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。
In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
在气动弹性,人们在设计过程
最为关心的是颤振现象。
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。
In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
在气动弹领域中,人们在设计过程中最为关心
振现象。
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了一种悬停状态下无铰旋翼桨叶气弹稳定
析方法。
声明:以上例句、词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。
In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
在气动弹性领域中,人们在设计过程中心的是颤振现象。
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了一种悬停状态下无铰旋翼桨叶气弹稳定性的分析
法。
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;若发现问题,欢迎向我们指正。
In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
在气动弹性领域中,人们在设计过程中最为是颤振现象。
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了一种悬停状态下无铰旋翼桨叶气弹稳定性
法。
声明:以上例句、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。