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1.
介绍了一种共轴双旋翼直升机的仿真建模方法及系统开发,包括整机动力学计算方法、旋翼拉力计算方法、基本飞行控制方法、仿真系统的组成以及程序开发。在旋翼拉力计算中采用了动态入流理论实现了气动载荷的实时计算,并针对共轴双旋翼及机体的气动耦合性提出了修正方法。系统主体及可视化程序采用OSG开源项目开发,而动力学计算程序采用C++编程语言设计,系统不依赖于第三方商业软件,且具有研发效率高、可视化效果好和扩展性好等特点。  相似文献   

2.
利用数值计算的方法对涡轮流量计内的三维湍流流动进行建模和基于N—S方程的仿真分析。数值计算采用k-ε模型来模拟湍流流动,得到涡轮流量计的内部流场三维流动形态,并分析其内部的流动规律、流速和压力分布;以三维湍流仿真的仿真结果为依据,对前导流器进行了优化。结果表明:流线型前导流器能降低整个流量计的压损。  相似文献   

3.
在单旋翼涵道尾桨直升机的非线性全量飞行动力学数值模型的基础上,提出了求解配平问题的一种混合算法,研究了地面效应对配平的影响。以某直升机为算例,在无地面效应和考虑不同悬停高度时,分别进行了初始参数进行了配平,配平计算结果与地面效应的理论相符合。  相似文献   

4.
水射流在工业生产中广泛应用,具有重要的研究价值。本文采用数值模拟方法,使用CFD软件对水射流的流场进行了模拟和分析。研究对圆形喷管进行了简化,建立了二维轴对称模型,流体介质为甘油水溶液,湍流模型基于SST-SAS模型,并与实验结果进行对比。研究发现,k-ε湍流模型在冲击射流低雷诺数区域的模拟能力不足,而SAS湍流模型在不同位置处的计算值与实验值吻合良好,表明该模型可以很好地模拟低雷诺数区域的冲击射流流场,可以为下一步研究冲击射流中冲击高度、喷嘴形状、雷诺数等因素对流动特性的影响奠定了良好的工作基础。  相似文献   

5.
<正>主要完成人:李家云、刘波、洪永军、危松林、黄文捷等主要完成单位:中国直升机设计研究所、昌河飞机工业(集团)有限责任公司该项目属于航空科学技术领域。主要技术内容和经济指标如下:1.创造性提出了"水滴形"直升机机身外形设计理念,开展了气动布局优化设计技术研究,形成了具有自主知识产权的低阻和高效的气动布局,全机阻力较国际先进同类直升机降低3.76%。2.旋翼系统采用高性能的主旋翼翼型,主旋翼采用高  相似文献   

6.
本文对侧伸式高浓度厌氧反应器流场进行了数值模拟,计算采用多重参考系法和标准k-ε湍流方程。模拟结果表明,由于高浓度流体具有牛顿流动特性,流体只在反应器底部形成了循环流动,在整个反应器内的湍流特性分布不均匀。在相同条件下,牛顿流体能够形成整体循环,湍流特性比较均匀。  相似文献   

7.
目的:液力缓速器高速运行时会产生气蚀侵蚀现象,进而对缓速器的缓速制动及平稳运行产生不利影响。本文旨在对液力缓速器的气蚀湍流场进行分析,探究气蚀侵蚀发生的原因,为进一步探究减轻气蚀侵蚀的措施提供理论基础。创新点:1.引入目前先进的尺度解析模拟方法来模拟湍流场,使湍流场数值计算结果更加真实;2.采用气液两相流模型和气蚀模型相结合的方法模拟气蚀现象,并通过流场中的气泡体积来衡量气蚀侵蚀程度。方法:1.采用不同的湍流模型解析液力缓速器四种转速下的湍流场,并通过比较流场结果得出不同湍流模型模拟流场的区别(图3~5和7);2.采用应力混合涡(SBES)模型模拟高转速下的气蚀流场,并提取流场处理结果来分析缓速器内部气泡体积的瞬态演变规律(图8和9);3.提取不同时刻的叶片温度来分析气蚀引起的能量变化(图12和13)。结论:1.在四大湍流模型中,SBES模型模拟湍流场涡旋的能力最强且提取出的制动转矩结果与实验值最接近;2.高转速下的气蚀侵蚀情况严重,流场中出现的气泡体积较大,并且,随着时间推移气泡体积累积对缓速器运行将产生不利影响。3.气蚀流场中出现的气泡会影响缓速器湍流场中的涡旋,并且影响缓速器的叶片温度变化。  相似文献   

8.
高浓度厌氧反应器流场的数值模拟   总被引:2,自引:1,他引:1  
本文对高浓度搅拌桨厌氧反应器流场进行了数值模拟,计算采用多重参考系法和标准k-ε湍流方程。模拟结果表明,与牛顿流体形成的单循环流动相比,在反应器内的非牛顿流体形成了两个循环流动,这不利于厌氧反应器内的混合。在整个反应器内的湍流特性分布不均匀,局部湍动比较剧烈。在设计高浓度厌氧反应器时应考虑非牛顿流体特性的影响。  相似文献   

9.
目的:探讨作用于大跨度曲面屋盖非定常气动力的特性,为考虑非定常气动力影响的大跨度曲面屋盖抗风设计提供理论参考。创新点:1.采用强迫振动试验;2.采用大涡模拟(LES)流入脉动风的生成方法;3.研究大跨度曲面屋盖非定常气动力特性。方法:1.通过强迫振动风洞试验方法探讨风速、强迫振动振幅、屋盖的矢跨比和缩减频率对非定常气动力的影响;2.采用计算流体力学数值模拟重现风洞试验,从而在更宽的缩减频率范围内分析非定常气动力的特性,并且通过可视化流场的分析探讨风与屋盖相互作用的机理。结论:1.屋盖的振动对屋盖表面的风压分布影响较大。2.屋盖的振动可能抑制屋盖背风面漩涡的脱落。3.根据风洞试验和数值模拟的结果分析得到的矢跨比、风速和振动振幅对气动阻尼系数和气动刚度系数的影响较小;气动阻尼系数和气动刚度系数主要随着缩减频率的变化而变化。4.气动刚度系数为正值,使得结构的总刚度减小,从而减小结构的固有频率;气动阻尼系数为负值,使得结构总阻尼增加。5.风洞试验和LES模拟结果的一致性可以说明,LES是一个能够有效研究非定常气动力特性的数值模拟方法。  相似文献   

10.
针对NACA4412翼型风力发电机扰流流动特点,建立了二维和三维不可压缩湍流模型,并对基于流体连续性方程和N-S方程及k-ε湍流模型的二维流场进行数值模拟计算。采用多参考系计算(MRF)模型,用FLUENT模拟了流场内翼型截面的受力情况和速度分布情况,得到了NACA4412翼型风机的气动特性。  相似文献   

11.
Fluent是流体力学中通用性较强的商业CFD软件。将Fluent软件引入流体力学多媒体教学中,可对定常不可压缩流体在圆管内流动进行数值模拟,分析流体层流、紊流的两种流动状态,验证管内流体速度及切应力分布。实践表明,在流体力学课堂上配以Fluent数值模拟,有助于学生消化较难理解的理论知识,增强学习兴趣,提高教学效果。  相似文献   

12.
This paper discusses the unsteady aerodynamic behavior of long-span vaulted roofs. First, a forced vibration test in a turbulent boundary layer is conducted in a wind tunnel. The models are force vibrated in the first anti-symmetric mode to investigate the effects of wind speed, rise/span ratio, and the amplitude and frequency of forced vibration on the distributions of wind pressures and unsteady aerodynamic forces. Then, a large eddy simulation (LES) is carried out to clarify the physical mechanism of wind-roof interaction as well as to investigate the influences of a roof’s vibration on the flow field around the roof. From the results of the wind tunnel experiment and the LES, we discuss the characteristics of unsteady aerodynamic forces on a long-span vaulted roof over a wide range of the reduced frequency of vibration. The effect of unsteady aerodynamic forces on the dynamic response of the roof is also discussed. A comparison between the wind tunnel experiment and the LES indicates that the LES can be used effectively to evaluate the unsteady aerodynamic behavior.  相似文献   

13.
建立了同向自洁双螺杆端面内二维周期性流动的物理模型及数学模型。借助商用有限元软件POLYFLOW叠加网格技术求解得到速度场,基于具有4阶精度的RungeKutta数值积分方法自行开发了流体前锋追踪代码,并对对混合过程动力学进行了数值模拟表征。采用粒子群可视化模拟、Poincaré截面分析、界面演化及界面增长等探讨了混合过程动力学细节,揭示混沌混合作用的尺度。结果表明,传统的同向双螺杆端面内混沌混合与常规的层流混合共存,不同区域的混合效果相差很大。螺槽中部存在8字型准周期运动带,带内混合为常规的层流混合。  相似文献   

14.
NUMERICALPROCEDUREFOR3DELLIPTICFLOWONNONSTAGGEREDGRIDSZhangHui(张辉)(ThermoenergyEngineeringResearchInstitute)ChenShannian(陈善年)...  相似文献   

15.
INTRODUCTION The use of dimethyl ether (DME) as an alterna-tive fuel appears to be a promising approach for si-multaneously minimizing NOx and soot emissionfrom conventional diesel engines. The lowself-ignition temperature of 508 K and the high oxy-gen content of 34.8 percent (mass fraction) are twomajor factors characterizing low soot and unburnedtotal hydrocarbon (THC) emissions. Since the firstintroduction of the concept by Sorenson and Mik-kelsen (19…  相似文献   

16.
Theoretical analysis and wind tunnel tests were carried out to study wind-induced intemal pressure response for the structure with single windward opening and background leakage. Its goveming differential equation was derived by the Bemoulli equation in an unsteady-isentropic form. Numerical examples were provided to study the additive damping caused by background leakage in laminar and turbulent flow, and the influence of background leakage on fluctuating internal pressure response was quantized. A series of models for low-rise building with various opening ratios and background leakage were designed and wind tunnel tests were conducted. It is shown that the fluctuating intemal pressure reduces when the background leakage are considered and that the effect of background leakage can be predicted accurately by the governing differential equation deduced in this paper.  相似文献   

17.
多功能流体流动实验装置   总被引:2,自引:1,他引:1  
在对流体流动阻力及离心泵特性曲线和管路特性曲线测定的基本原理分析研究基础上,自主设计并制作了多功能流体流动实验装置。该实验装置既可进行层流和湍流流型下流体流动阻力的测定,还可以进行不同转速下的离心泵特性曲线和管路特性曲线的测定,从而一方面使设备的制作、维护成本和实验用房面积大大降低,另一方面学生的受训效率大大增加。  相似文献   

18.
Temporal mode direct numerical simulation was done for the process of laminar-turbulent transition in an incompressible boundary layer on a flat plate. The analysis of the results showed that during the breakdown process of laminar-turbulent transition, the modification of the mean flow profile by the disturbances led to a remarkable change in its stability characteristics, manifested in the significant enlargement of the linear unstable zone and the maximum amplification rate, and led to that many more disturbances were excited and enhanced rapidly, correspondingly the turbulent energy also increased rapidly, and the mean flow profiles evolved swiftly from laminar to turbulent. It was also found that if the oblique waves in the initial disturbances did not form symmetrical pairs, the subsequent span-wise mean velocities would, in general, be nonzero due to nonlinear interaction, which would have a great effect on the stability characteristics and also implied that the turbulence obtained by direct numerical simulation might not be fully a random process.  相似文献   

19.
Particle image velocimetry (PIV) experimental results of wake flow structure of a NACA0012 airfoil with small attack angle mounted above water surface are introduced.The experiment was carried out in a small-scale wind-wave tunnel.The diameter of wind-wave tunnel test section is 1.7 m (long) × 0.4 m (width) × 0.4 m (height).The flow fields around the airfoil were measured under four diffierent conditions by varying the distance between the airfoil and the water surface.The attack angle of the airfoil was kept 10- during the experiment.For each experimental condition,the time series of particle images was captured to calculate continuous evolution of the velocity fields.The velocity fields were ensemble averaged to get the statistic parameters such as mean velocity and vorticity.Typical instantaneous velocity fields for each case are introduced to show the basic flow structure of wind surface flow separation.The aerodynamic loads acting on the airfoil are analyzed qualitatively according to the mean vorticity distribution in the flow field based on the theory of vorticity aerodynamics.The results indicate that the flow structures and drag/lift force of the airfoil alter remarkably with the changing distance between the airfoil and water surface.  相似文献   

20.
Short path distillation (SPD) is a kind of high vacuum distillation method, which is suitable for the separation of high boiling, heat sensitivity and viscidity products.In this paper,through measuring the phase-averaged velocity distributions with a conditional sampling method of the particle imaging velocimetry (PIV), the liquid flow field that affects the heat and mass transfer of evaporating thin-film in an SPD evaporator is investigated.Measured results show that the flow velocities decrease rapidly apart from the wiper at different wiper velocities, the maximum velocity appears before wipers, and the quicker the wiping, the larger the flow velocity. Meanwhile, the evaluation of numerical calculations is carried out.The measured velocity distributions indicate clearly the effect of the wiper both on the flow field along its moving direction and on the vortices behind the wiper.Simulation data show that the performance of liquid flow field on the heating surface not only agrees with the experimental results well,but also can give further more information, such as the distribution of turbulent kinetic energy.In this study,turbulent kinetic energy mainly distributes before wipers and laminar flow appears far away from the wipers.  相似文献   

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