Except the centralized load impressed from plane other components and airload, the plane gun bay structure is also endured the wallop of the navigate gun launching.
在行过程中,炮舱结构除承受
它零部件传递的集中载荷和空气气动载荷外,还要承受航炮发
时的冲击
,整个结构始终处于不规则的振动状态。
Except the centralized load impressed from plane other components and airload, the plane gun bay structure is also endured the wallop of the navigate gun launching.
在行过程中,炮舱结构除承受
它零部件传递的集中载荷和空气气动载荷外,还要承受航炮发
时的冲击
,整个结构始终处于不规则的振动状态。
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.
基于桨叶二线理论和旋翼自由尾迹模型,本文在第三章建立了一个适合于直
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、词性分类均由互联网资源自动生成,部分未经过人工审核,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。
Except the centralized load impressed from plane other components and airload, the plane gun bay structure is also endured the wallop of the navigate gun launching.
在机
行过程中,炮舱结构除承受
机其它零部件传递的集中载荷和空气气动载荷外,还要承受航炮发
时的冲击力,整个结构始终处于不规则的振动状态。
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由尾迹模型,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-气动特性分析的方法和模型。
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。
Except the centralized load impressed from plane other components and airload, the plane gun bay structure is also endured the wallop of the navigate gun launching.
机
行过程中,炮舱结构除承受
机其它零部件传递的集中载荷和空气气动载荷外,还要承受航炮发
时的冲击力,整个结构始终处于不规则的振动状态。
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由尾迹模型,本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。
Except the centralized load impressed from plane other components and airload, the plane gun bay structure is also endured the wallop of the navigate gun launching.
机
行过程中,炮舱结构除承受
机其它零部件传递的集中载荷和空气气动载荷外,还要承受航炮发
时的冲击力,整个结构始终处于不规则的振动状态。
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由尾迹模型,本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。
Except the centralized load impressed from plane other components and airload, the plane gun bay structure is also endured the wallop of the navigate gun launching.
在飞机飞行过程中,炮舱结构除承受飞机其它零部件传递的集中载荷和空气气载荷外,还要承受航炮发
时的冲击
,整
结构始终处于不规则的振
状态。
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.
基于桨叶二阶升线理论和旋翼自由尾迹模型,本文在第三章建立了
合于直升机旋翼尾迹结构及桨-涡干扰气
特性分析的方法和模型。
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。
Except the centralized load impressed from plane other components and airload, the plane gun bay structure is also endured the wallop of the navigate gun launching.
在飞机飞行过程中,舱结构除承受飞机其它零部件传递
集中载荷和空气气动载荷外,还要承受航
冲击力,整个结构始终处于不规则
振动状态。
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由尾迹模型,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方法和模型。
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观点;若
现问题,欢迎向我们指正。
Except the centralized load impressed from plane other components and airload, the plane gun bay structure is also endured the wallop of the navigate gun launching.
在行过程中,炮舱结构除承受
其它零部件传递的集中载荷和空气气动载荷外,还要承受航炮发
时的冲击力,整个结构始终处于不规则的振动状态。
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自由尾迹模型,本文在第三章建立了一个适合于直升
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。
Except the centralized load impressed from plane other components and airload, the plane gun bay structure is also endured the wallop of the navigate gun launching.
在飞飞行过程中,炮舱结构除承受飞
其它零部件传递
集中载荷和空气气动载荷外,还要承受航炮发
时
冲击力,整个结构始终处于不规则
振动状态。
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.
基于桨叶二阶力线理论和旋
自由尾迹模型,本文在第三章建立了一个适合于
旋
尾迹结构及桨-涡干扰气动特性分析
方法和模型。
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观点;若发现问题,欢迎向我们指正。
Except the centralized load impressed from plane other components and airload, the plane gun bay structure is also endured the wallop of the navigate gun launching.
在飞机飞行过程中,舱结构除承
飞机其它零部件传递
集中载荷和空气气动载荷外,还要承
发
时
力,整个结构始终处于不规则
振动状态。
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由尾迹模型,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方法和模型。
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观点;若发现问题,欢迎向我们指正。