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
分析
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
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.
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
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
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
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
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
权
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-涡干扰气动特性分析的方法和模型。
声明：以
、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
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。
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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
悬停状态下无铰旋翼桨叶气弹稳定性
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，本文在第三章建立个适合于直升机旋翼尾迹结构及桨-涡干扰气动特性方法和模型。
声明：以上例句、词性
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.
基于桨叶二阶升力线
旋翼自尾迹模
，
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模。
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。
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.
基于二阶升力线理论和旋翼自尾
模型，本文在第三章建立了一个适合于直升机旋翼尾
及-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,