In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
气动弹
领域中,
设计过程中最为关心的是颤振现象。
In the domain of aeroelastics, flutter phenomenen is paid most attention when designing aircraft.
气动弹
领域中,
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
的
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
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
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
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
的分析方法。
声明:以上例句、词分类均由互联网资源自动生成,部分
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法发
了
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法发
了一
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
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
分析方法。
声明:以上例句、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
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.
在动
性领域中,人们在设计过程中最为关心的是颤振现
。
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
了一种悬停状态下无铰旋翼桨
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。