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
停状态下无铰旋翼桨叶气弹稳定
的
方法。
jiǎng yè
- awe
- paddle
In Chapter 3, based upon the blade second-order lifting-line model and rotor free-wake model, an analytical method is developed for predicting the rotor wake structure and BVI airload.
基于桨叶二阶升力线理论和旋翼自
尾迹模型，本文在第三章建立了个适合于直升机旋翼尾迹结构及桨-涡干扰气动特的方法和模型。
声明：以上例句、词
类均
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。
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桨轮, 桨片, 桨手, 桨手坐板, 桨形的, 桨叶, 桨叶柄, 桨叶扭旋, 桨叶式装载机, 桨叶形三角洲,
jiǎng yè
- awe
- paddle
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。
In Chapter 3, based upon the blade second-order lifting-line model and rotor free-wake model, an analytical method is developed for predicting the rotor wake structure and BVI airload.
基于桨叶二阶升力线理论和旋翼自
尾迹
，本文在第三章建立了一个适合于直升机旋翼尾迹结构及桨-涡干扰气动特性分析的方法和。
明：以上例句、词性分类均
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。
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桨轮, 桨片, 桨手, 桨手坐板, 桨形的, 桨叶, 桨叶柄, 桨叶扭旋, 桨叶式装载机, 桨叶形三角洲,
jiǎng yè
- awe
- paddle
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。
In Chapter 3, based upon the blade second-order lifting-line model and rotor free-wake model, an analytical method is developed for predicting the rotor wake structure and BVI airload.
基于桨叶二阶升力
和旋翼自尾迹模型，
第三章建立了一个适合于直升机旋翼尾迹结构及桨-涡干扰气动特性分析的方法和模型。
声明：以上例句、词性分类均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。
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桨轮, 桨片, 桨手, 桨手坐板, 桨形的, 桨叶, 桨叶柄, 桨叶扭旋, 桨叶式装载机, 桨叶形三角洲,
jiǎng yè
- awe
- paddle
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
了一种悬停状态下无铰旋翼桨叶气弹稳定性的分析
法。
In Chapter 3, based upon the blade second-order lifting-line model and rotor free-wake model, an analytical method is developed for predicting the rotor wake structure and BVI airload.
基于桨叶二阶升力线理论
旋翼自尾迹模型，本文在第三章建立了一个适合于直升机旋翼尾迹结构及桨-涡干扰气动特性分析的法模型。
声明：以上例句、词性分类均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
现问题，欢迎向我们指正。
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桨轮, 桨片, 桨手, 桨手坐板, 桨形的, 桨叶, 桨叶柄, 桨叶扭旋, 桨叶式装载机, 桨叶形三角洲,
jiǎng yè
- awe
- paddle
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析方法。
In Chapter 3, based upon the blade second-order lifting-line model and rotor free-wake model, an analytical method is developed for predicting the rotor wake structure and BVI airload.
基于桨叶二阶升力线理论和旋翼自尾迹模型，本文在第三章建立了一个适合于直升机旋翼尾迹结构及桨-涡干扰气动特性析的方法和模型。
声明：以上例句、词性
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。
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桨轮, 桨片, 桨手, 桨手坐板, 桨形的, 桨叶, 桨叶柄, 桨叶扭旋, 桨叶式装载机, 桨叶形三角洲,
jiǎng yè
- awe
- paddle
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
稳定性的分析方法。
In Chapter 3, based upon the blade second-order lifting-line model and rotor free-wake model, an analytical method is developed for predicting the rotor wake structure and BVI airload.
基于桨二阶升力线理论和旋翼自
模型，本文在第三章建立了一个适合于直升机旋翼
构及桨-涡干扰动特性分析的方法和模型。
声明：以上例句、词性分类均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。
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桨轮, 桨片, 桨手, 桨手坐板, 桨形的, 桨叶, 桨叶柄, 桨叶扭旋, 桨叶式装载机, 桨叶形三角洲,
jiǎng yè
- awe
- paddle
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
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的析方法。
In Chapter 3, based upon the blade second-order lifting-line model and rotor free-wake model, an analytical method is developed for predicting the rotor wake structure and BVI airload.
基于桨叶二阶升力线理论和旋翼自尾迹模型，本文在第三章建立了一个适合于直升机旋翼尾迹结构及桨-涡干扰气动特析的方法和模型。
声明：以上例句、词均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。
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桨轮, 桨片, 桨手, 桨手坐板, 桨形的, 桨叶, 桨叶柄, 桨叶扭旋, 桨叶式装载机, 桨叶形三角洲,
jiǎng yè
- awe
- paddle
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
种悬停状态下无铰旋翼桨叶气弹稳定性
分法。
In Chapter 3, based upon the blade second-order lifting-line model and rotor free-wake model, an analytical method is developed for predicting the rotor wake structure and BVI airload.
基于桨叶二阶升力线理论和旋翼自尾迹模型，本文在第三章建立个适合于直升机旋翼尾迹结构及桨-涡干扰气动特性分法和模型。
声明：以上例句、词性分类均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。
用户正在搜索
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桨轮, 桨片, 桨手, 桨手坐板, 桨形的, 桨叶, 桨叶柄, 桨叶扭旋, 桨叶式装载机, 桨叶形三角洲,
jiǎng yè
- awe
- paddle
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的析方法。
In Chapter 3, based upon the blade second-order lifting-line model and rotor free-wake model, an analytical method is developed for predicting the rotor wake structure and BVI airload.
基于桨叶二阶升力线理论和旋翼自尾迹模型，本文在第三章建立了一个适合于直升机旋翼尾迹结构及桨-涡干扰气动特析的方法和模型。
声明：以上例句、词均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。
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桨轮, 桨片, 桨手, 桨手坐板, 桨形的, 桨叶, 桨叶柄, 桨叶扭旋, 桨叶式装载机, 桨叶形三角洲,