可用于表面压力分布以及描述翼型边界层流的。
Surface pressure distribution can be used to describe the airfoil boundary layer flow well.
表面压力分布对断面的气动特性有着重要的影响。
The surface pressure distribution around the deck section has significant influence on the aerodynamic behaviour of the deck.
并给出了模型表面压力随声压级及频率变化的规律。
Regularities of pressure on surface with sound pressure level and frequency are also given.
根据所测非平衡张力，对应动态表面压力数据也进行了计算。
The dynamic surface pressure was obtained according to experimental data.
桥梁断面表面压力系数、最小压力系数等是桥梁断面重要的参数。
The surface pressure coefficient and the minimum pressure coefficient of a bridge deck section are important parameters of the bridge.
本文对一台单级轴流压气机静子叶片非定常表面压力进行了测量。
The unsteady surface pressure on stator blade of an axial compressor was measured by means of mounting micro-sensors on blades surface.
方法是直接的，即由给定物体形状可求出表面压力分布和激波形状。
This method is direct, in that it gives the surface-pressure distribution and shock shape for a prescribed body.
本文介绍了可用于测量风洞中旋转模型表面压力分布的集成测试系统。
The paper introduced a spinning model surface pressure measurement sy which used in the wind tunnel.
本文利用积分变换方法求解皮肤层在表面压力作用下的蠕变响应问题。
The creep of a skin layer under a distributed surface pressure was solved by an analytical method using Hankel transform and Laplace transform.
由于叶排间的相互运动，使叶片表面压力和叶栅通道内的流场呈周期性地变化；
Because of relative movement of blade rows, the pressure distributions on the blade and the flow field in the cascade vary periodically.
着重分析影响精密分度装置寿命的接触表面压力，基本动载荷，温度系数等因素。
This article mainly analyses the factors that affect the precise indexer life, touching surface pressure, basic motion load and temperature factor for example.
本文提供了一种根据升力面理论计算螺旋桨桨叶表面压力分布和螺旋桨性能的数值方法。
A numerical method is presented for prediction of propeller performance and pressure distribution on blade surface according to lifting surface theory.
试飞结果表明，机翼蒙皮直接改装测量孔和测压带方法均能有效测量机翼表面压力分布。
The flight test results show that the Stripe-A-Tube method is as more effective as measurement that transform hole of static pressure on wing surface.
试飞结果表明，机翼蒙皮直接改装测量孔和测压带方法均能有效测量机翼表面压力分布。
The flight test results show that the Stripe-A-Tube method is as more effective as measurement that transform hole of sta…
尽管该风洞的尺寸很小，我们仍对翼型表面压力分布试验段的研制工作进行了大胆的尝试。
Although it is very small in size, some developments in the test section of pressure distribution on airfoil surface have been attempted.
结果表明：车体迎风面及背风面表面压力分布规律基本一致，验证了数值模拟计算模型的准确性；
The results show that the pressure distribution on external surface at both windward and leeward is basically the same.
结果表明：车体迎风面及背风面表面压力分布规律基本一致，验证了数值模拟计算模型的准确性；
Numerical computation was carried out by FLUENT for the test train passing by the east of "Mengjin", and the computation result was compared with that of the real vehicle measurement.
通过对旋转风机叶片表面压力信号测量的应用，介绍了风机实验台的信号光电转换系统的结构及原理；
The theory and structure of the opt-electronic pressure measuring and transferring system are introduced, which has been used in measuring static pressure of the rotating centrifugal fan successfully.
通过计算得到的舵表面压力分布可看出反应舵节能的原因。本文还对反应舵的操纵性能进行了计算和研讨。
The pressure distribution on rudder surface and the hydrodynamic performance ofthe reaction rudder are discussed in the paper.
介绍了国内首次在高速风洞中使用荧光压力传感器(LPS)技术对飞机模型机翼表面压力场测量的初步结果。
The pressure field measurement results on the wing surface of airplane model by luminescence pressure sensor (LPS) technique and classic tap technique in high speed wind tunnel are presented.
在风洞实验中采用纹影照相和压力分布相结合的实验方法，确定了侧后向喷流复合增程技术中喷嘴—模型之间间隙的大小对表面压力的影响。
The influence of clearance between the nozzles and the model of the surface pressure was used in the hybrid extended-range technique of the side back jet.
对试验列车上、下行通过“猛进东”测风点时的车体表面压力分布情况进行分析，采用分块积分法得出试验列车上、下行通过“猛进东”测风点的气动力。
The pressure distribution on external surface of the test vehicle was analyzed when it passed the anemology station on the east of "Mengjin" from upward and downward.
通常将垂直柱体在波浪场中的受力分为正向力(顺流力)与升力，它们是由干粘性流绕钝体产生的摩擦阻力和由于水流绕柱分离产生涡漩而形成柱表面压力分布的不均匀变化而造成的。
When waves act on a vertical cylinder, there are in-line and lift forces. They are caused by the viscous effect, which induces the surface frictional force and flow separation and vortex shedding.
压力必须均匀分布于整个表面。
Pressure must be uniformly distributed over the whole surface.
这是因为磁场降低了施加在内部气体上的压力，使得太阳黑子比太阳表面的其他部分温度更低。
That's because magnetic fields reduce the pressure exerted on the gases inside of them, making the spots cooler than the rest of the Sun's surface.
一旦水滴流到了圆锥体的边缘，就会在锥体表面张力所形成的压力差的作用下流向它的底座，那里是曲线弧度最小的地方。
Once they hit the edge of a cone, drops are propelled towards its base, the least curved region, because of the pressure difference caused by surface tension.
在气态表层之下，它们并没有固体的表面——外层大气产生的压力融化了它们的内部，尽管它们可能具有石质的核心。
Beneath these outer layers, they have no solid surfaces - the pressure from their thick atmospheres liquefy their insides, although they might have rocky cores.
在气态表层之下，它们并没有固体的表面——外层大气产生的压力融化了它们的内部，尽管它们可能具有石质的核心。
Beneath these outer layers, they have no solid surfaces - the pressure from their thick atmospheres liquefy their insides, although they might have rocky cores.
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