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
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
桨叶二阶
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
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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相似单词
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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Informix, informofer, informosome, infortune, infotainment, INFOTERM, Infotom, infra, infra-, infra dig,
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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
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
模型，本文在第三章建立了一个适合于直升机旋结构及桨-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
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
种悬停状态下无铰旋翼
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.
基二阶升力线理论和旋翼自尾迹模型，本文在第三章建
个适合直升机旋翼尾迹结构及-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
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
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。
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种悬停状态下无铰旋翼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.
叶二阶升力线理论和旋翼自尾迹模型，本文在第三章建立
适合直升机旋翼尾迹结构及-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本软件的观点；若发现问题，欢迎向我们指正。
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infraspinatus, infrasplenic, infrasternal, infrastructure, infrastucture, infrategillar, infratonsillar, infratracheal, infraversion, infrequence,
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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：以上句、词性分类均互
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。
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
升机旋翼尾迹结构及桨-涡干扰气动特性的法和模型。
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,