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弹性机翼与英语短句例句大全

时间:2019-04-04 18:54:02

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The concept of an "elastic wing" has generated considerable interest in the field of aeronautical engineering, representing a cutting-edge approach to aircraft design. The use of elastic materials in wing construction allows for dynamic flexibility and shape adaptation, leading to improved aerodynamic performance and fuel efficiency. This approach is revolutionizing the design and operation of aircraft, promising to enhance maneuverability, reduce structural weight, and minimize environmental impact. The following collection of English short sentences and example sentences related to "elastic wing" provides a comprehensive overview of this innovative technology, offering insights into its potential applications and benefits in the aviation industry.

弹性机翼,elastic wing

1)elastic wing弹性机翼

1.Numerical simulation on gust response ofelastic wing弹性机翼阵风响应数值计算方法

2.A new approach using control theory for the aerodynamic optimization design ofelastic wing where aeroelastic interactions are significant is implemented and tested.耦合流场控制方程和结构静平衡方程求解得到大展弦比跨声速弹性机翼气动性能,分析研究了结构静弹性变形对气动载荷的影响。

英文短句/例句

1.INDUCED DRAG REDUCTION OPTIMIZATION STUDY USING MULTI-CONTROL SURFACES FOR ELASTIC WING减小弹性机翼诱导阻力的多控制面优化研究

2.Review of Aeroelastic Stability Investigations for Tiltrotor Aircraft倾转旋翼机气动弹性稳定性研究进展

3.A Static Aeroelastic Numerical Analytic Method of Transonic Flow About Wings跨声速机翼静气动弹性数值分析方法

4.Topology Optimization Design of Wing Scale-Model;机翼弹性比例模型结构拓扑优化设计

5.The Nonlinear Aeroelastic Analysis of Wings Based on CFD/CSD;基于CFD/CSD的机翼非线性气弹分析

弹性机翼与英语短句例句大全

6.Analysis of the nonlinear aeroelastic response for large-aspect-ratio wing大展弦比机翼的非线性气弹响应分析

7.Modeling study on tilt-rotor"s aeroelastic stability in cruise flight前飞状态倾转旋翼机气弹稳定性建模

8.Random uncertainty of aeroelastic system机翼气动弹性的随机不确定性分析研究

9.STATIC AEROELASTIC CHARACTERISTICS ANALYSIS OF A FLEXIBLE FORWARD-SWEPT COMPOSITE AIRCRAFT柔性复合材料前掠翼飞机静气动弹性分析

10.Study of aeroelastic tailoring of high-aspect-ratio flexible composite wing大展弦比柔性复合材料机翼的气动弹性剪裁

11.An Aeroelastic Analysis Method of Wings Based on Euler Equations基于欧拉方程的一种机翼气动弹性计算方法

12.Study on Some Aeroelastic and Stability Analyses of Tiltrotor;倾转旋翼机气弹响应及稳定性若干问题研究

13.Mechanism Study and Function Analysis of Wind-Corrected Munition Dispenser Tail-Kit;风修正弹药尾翼组件机理研究及性能分析

14.Nonlinear Aeroelastic Response and Flutter Analysis of High-Aspect-Ratio Wings;大展弦比机翼的非线性气弹响应与颤振分析

15.Dynamic model of elastic impact of helicopter rotor blades直升机旋翼桨叶的弹性碰撞动力学建模

16.Structural Layout Optimization of Aircraft Wing under Aeroelastic Constrains考虑气动弹性约束的机翼结构布局优化设计

17.CALCULATION OF AERODYNAMIC CHARACTERISTICS WITH EXISTENCE OF THE BOMB-WING-BODY CONFIGURATION DISTURBANCE弹-翼-机身组合体干扰条件下航弹的气动特性计算

18.aerodynamic characteristics of winged missile有翼导弹空气动力特性

相关短句/例句

Active aeroelastic wing主动气动弹性机翼

1.Active aeroelastic wing (AAW) technology is a new idea in modern aircraft design, and active flutter suppression and gust alleviation for multi input/multi output systems is the main research aspect in AAW.多输入 /多输出系统的颤振主动抑制与阵风减缓是主动气动弹性机翼技术的重要研究方面。

3)Wing scale-model机翼弹性比例模型

4)bomb-wing-body configuration弹-翼-机身组合体

5)expanding mechanism of missile wing弹翼展开机构

6)missile wing弹翼

1.It is shown that the scheme of the aerodynamic simulation load device is practicable;the aerodynamic loads ofmissile wings can be simulated in a practical and equivalent way,which may greatly reduce the time and expense for related development.实践应用表明气动模拟加载装置方案基本能够真实、等效的模拟弹翼气动载荷,利用该装置大大地缩短研制周期、节省研制经费,可以进行推广应用。

2.Formissile wing,introduce its computation model,load conditions,development plan,test circuit,test results etc.介绍了弹翼展开装置的计算模型、载荷条件、研制方案、测试电路、试验结果等,在地面模拟确定弹翼展开过程中所需的气动力参数,从而优化了作动筒参数,保证了弹翼的顺利展开。

3.The high real-time requirement of the spreading ofmissile wing requires that electric loading system be used.基于实时性要求极高的导弹弹翼电动加载系统的硬件结构和控制原理,对多余力矩的产生原因、理论计算及消除方法进行了详细研究。

延伸阅读

弹性分子式:CAS号:性质:除去导致变形的负荷以后,材料迅速回复其原来尺寸和形状的能力。当变形与所加负荷成正比时,该材料被认为是虎克弹性体或理想弹性体。应力和应变不满足线性关系,但仍保持单值关系称非线弹性。加载后经过一定时间后应力和应变才满足线性关系称滞弹性。

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