aerodynamic的例句大全

The Effect Of Volute Throat Gap In Cross Flow Fans of Air-Conditioning On Aerodynamic Characteristics

分体空调室内体贯流风机蜗舌间隙对气动特性的影响

Mechanism of centrifugal blower creating aerodynamic noise is analyzed, and the methods for noise reduction by optimizing structure parameters such as volute throat gap, volute throat radial and relative width of swirl regions in exit blade channel are put forward.

分析了通风机空气动力噪声产生的机理，提出通过优化风机的蜗舌间隙、蜗舌半径以及叶道出口涡流区相对宽度等关键结构参数降低噪声的方法。

A numerical simulation study is conducted of the aerodynamic field characteristics of a 1000 t/ h once through boiler double furnace.

本文对1000t／h直流炉单炉体双炉膛的炉内空气动力场进行了数值模拟研究。

Analysis of Transition Interface Affecting Test Result of Aerodynamic Performance for Through-flow Fan

过渡接口对贯流风机气动特性测试结果影响的分析

The Investigation of the Influence of Thrust Vectoring Jet Flow on Aircraft Aerodynamic Load

矢量推力喷流对飞行器气动载荷影响的研究

Different from general jet flow, thrust vectoring jet flow has a vectoring angle, which greatly contributes to the aerodynamic interference.

与普通喷流相比，矢量推力喷流具有喷流偏转的特点，喷流偏转对气动干扰有重要贡献。

Thrust vectoring jet flow interferes the flow over aircrafts, drives its aerodynamic load to vary, and may potentially influence the controllability of aircrafts.

矢量推力喷流对飞行器绕流具有干扰作用，引起飞行器气动载荷变化，对飞行器操纵性也有潜在影响。

This paper analyzes the different factors influencing the runway operation. Through building aerodynamic, thrust, and runway surface models combined with kinematics and using object-oriented computer language, the simulation of runway operation is realized in meeting the minimum air traffic control separation requirement.

分析了影响跑道运行的各种因素，通过建立气动、推力、道面等数学模型，结合运动学方法，采用面向对象的计算机语言实现了在最小空管间隔下跑道运行的仿真。

The development of higher efficiency and larger thrust-weight ratio of aeroengine has put a further demand on the aerodynamic performance of compressor component.

航空发动机的高效率以及高推重比的发展方向对压气机部件性能提出了更高的要求。

Flow visualization in the wind tunnel using colour helium bubbles has been achieved at Harbin Aerodynamic Research Institute in March, 1984.Rich and varied paths were obtained. Clear colour video tape recording and colour photographs were taken.

在风洞中应用彩色氦气泡进行流动显示已于1984年3月在哈尔滨空气动力研究所实现了，获得了丰富多采的彩色迹线，摄制了清晰的彩色录象和彩色照片。

Calculation of the Aerodynamic Interaction between Rotor/ Wing/ Fuselage of Tilt-Rotor; the sleek swept wings of the plane.

倾转旋翼飞行器旋翼/机翼/机身气动干扰计算飞机有后掠翼的圆滑的机翼。

A discussion on the influence of air film on the back of bushing for tilting bushed aerodynamic bearing

可倾瓦气体动压轴承瓦背气膜影响的探讨

Study on Aerodynamic Bearing Elastically Supported by Tilting Pad

弹性支承可倾瓦气体动压轴承动特性和稳定性研究

We can according to the requirements of users design and manufacture the most perfect aerodynamic products.

我们可根据用户的要求设计制造各种最完美的气动产品。

Effects of squealer tips on blade aerodynamic performances and tip heat transfer in a gas turbine were investigated.

应用数值方法研究了燃气透平动叶顶部凹槽对动叶气动性能及叶顶传热的影响。

The angular motion of the models during the quasi-steady flow was recorded by synchroflash and the aerodynamic stability coefficients were derived from the motions by parameter differential method.

采用同步高速摄影方法记录了20ms准定常试验时间中模型的角运动并用参数微分法进行气动参数辨识。

Influence of the Backward Jet of Afterbody on the Aerodynamic Characteristic of Forebody During Stage Separation

级间分离过程中后体反向喷流对前体气动特性的影响

Aerodynamic heating problems are the key to the design of hypersonic vehicle TPS ( Thermal Protection System).

气动加热问题是高超声速飞行器TPS（Thermal Protection System，热防护系统）设计的关键，数值模拟是研究气动加热问题的重要手段，对气动热数值模拟进行研究具有重要的意义。

By using the rotor wing experimental equipment, experimental investigation about the influent factors on nozzle jet reacting force is carried on, and the validity of the primary evaluating method for rotor wing aerodynamic performance is verified furthermore.

利用旋转机翼地面试验装置开展了喷口喷气反作用力影响因素的试验研究，并进一步验证了旋转机翼垂直飞行基本气动性能的初步估算方法的有效性。

With the tool of Visual C++, the aerodynamic damping and structure reaction modules of the blade are developed.

采用Visual c++开发工具，开发出了气动阻尼及叶片结构响应模块。