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下无铰旋翼桨叶气弹稳定性的分析
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下无铰旋翼桨叶气弹稳定性的分析
法。
The contact between welding plate and fixture is treated as constraint in the finite element model of dynamic welding angular distortion simulation for overlayer in CO2 gas arc welding.
要采用有限元数值模拟
法
究了CO2气体保护堆焊的角变形
程。为了反映夹具和焊接件的接触状
,将夹具和焊件统一建立有限元模型。
声明:以上例句、词性分类均由互联网资源自生成,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。
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。
The contact between welding plate and fixture is treated as constraint in the finite element model of dynamic welding angular distortion simulation for overlayer in CO2 gas arc welding.
摘要采用有值模拟方法
究了CO2气体保
的角变形动态过程。为了反映夹具和
接件的接触状态,将夹具和
件统一建立有
模型。
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。
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.
采用伽辽金加权有限
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。
The contact between welding plate and fixture is treated as constraint in the finite element model of dynamic welding angular distortion simulation for overlayer in CO2 gas arc welding.
摘要采用有限值
拟方法
究了CO2气体保护堆焊的角变形动态过程。为了反映夹具和焊接件的接触状态,将夹具和焊件统一建立有限
。
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。
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法。
The contact between welding plate and fixture is treated as constraint in the finite element model of dynamic welding angular distortion simulation for overlayer in CO2 gas arc welding.
摘要采用有限元数值模拟法
究了CO2气体保护堆焊的角变形动态
。
了反映夹具和焊接件的接触状态,将夹具和焊件统一建立有限元模型。
声明:以上例句、词性类均由互联网资源自动生成,部
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。
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无铰旋翼桨叶气弹稳定性的分析方法。
The contact between welding plate and fixture is treated as constraint in the finite element model of dynamic welding angular distortion simulation for overlayer in CO2 gas arc welding.
摘要采用有限元数值模拟方法究了CO2气体保护堆焊的角变形动
过程。为了反映夹具和焊接件的接触
,
夹具和焊件统一建立有限元模型。
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。
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.
采用伽辽金加权余有限
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。
The contact between welding plate and fixture is treated as constraint in the finite element model of dynamic welding angular distortion simulation for overlayer in CO2 gas arc welding.
摘要采用有限模拟方法
究了CO2气体
焊的角变形动态过程。为了反映夹具和焊接件的接触状态,将夹具和焊件统一建立有限
模型。
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。
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。
The contact between welding plate and fixture is treated as constraint in the finite element model of dynamic welding angular distortion simulation for overlayer in CO2 gas arc welding.
摘要采用有限数值模拟方法
究了CO2气体保护堆焊的角变形动态过程。为了反映夹具和焊接件的接触状态,将夹具和焊件统一
有限
模型。
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。
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。
The contact between welding plate and fixture is treated as constraint in the finite element model of dynamic welding angular distortion simulation for overlayer in CO2 gas arc welding.
摘要采用有限元数值模拟方法究了CO2气体保护堆焊的角变形动态过程。为了反映夹具和焊接件的接触状态,将夹具和焊件统一建立有限元模型。
声明:以上句、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发展了一种悬停状态下无铰旋翼桨叶气弹稳定性的析方法。
The contact between welding plate and fixture is treated as constraint in the finite element model of dynamic welding angular distortion simulation for overlayer in CO2 gas arc welding.
摘要采用有限元数值模拟方法究了CO2气体保护堆焊的角变形动态过程。为了反映夹具和焊接件的接触状态,将夹具和焊件统一建立有限元模型。
声明:以上、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。