首页 | 本学科首页   官方微博 | 高级检索  
相似文献
 共查询到20条相似文献,搜索用时 125 毫秒
1.
为研究基于等离子流动控制的减阻技术,基于Langtry-Menter转捩模型提出边界层转捩数值模拟技术.该技术可有效结合转捩模型与湍流模型,用标准模型验证其精确性,为采用等离子流动控制抑制边界层分离和转捩研究提供数值模拟平台.采用基于现象学模型的等离子流动控制数值模拟技术,对流动分离以及边界层转捩抑制进行数值模拟,为基于等离子流动控制的翼型减阻技术提供参考.  相似文献   

2.
研究混压式超声速进气道改善阻力性能问题,改变进气道构型,针对Kantrowitz极限标准在进气道收缩比的设计上都过于保守;针对粘性效应问题,通过改进方法来控制激波/边界层干扰所造成的边界层分离现象,可以有效的降低粘性效应所带来的负面影响,提高进气道的起动特性,设计点和非设计点(Ma=3.5)均能达到优化进气道性能指标的效果.应用CFD对超声速进气道的起动特性进行了数值仿真分析,并从定量角度给出了如何施加壁面开缝措施来控制进气道的边界层分离现象.仿真结果发现在无粘和粘性条件下,相对开缝前,进气道的总压恢复系数分别提升了8.1%和22.7%.同时仿真结果表明,对于超声速进气道的设计和改进有一定的指导作用.  相似文献   

3.
艇身外形优化设计是平流层飞艇减阻的有效方法之一,艇身转捩尤其是横流转捩对于三维艇身的阻力特性有很大影响.采用SST-k-ω湍流模型耦合添加了横流修正的γ-Reθ-CF转捩模型在高精度CFD软件平台上进行艇身绕流计算.首先针对标准6:1椭球体算例进行数值方法验证,结果表明γ-Reθ-CF转捩模型能够比原始模型更好地预测旋成体外形的转捩位置,对于阻力特性的描述较为准确,且能够反映不同迎角下横流效应对旋成体外形转捩的影响.在此基础上,开展了考虑横流效应的艇身外形优化研究,涉及的几何因素包括艇身长度,艇身长细比和艇身最大直径的位置.选取传统的Goodyear飞艇艇身为参考,优化后的艇身在0°迎角下的总阻力减少约40%.  相似文献   

4.
在小型低速风洞中开展了一系列纵向脊状表面与光滑平板表面湍流边界层猝发频率检测研究,并获得了典型纵向脊状表面湍流猝发频率特性.试验在一小型低速风洞中开展,流场测试中使用恒温式IFA300智能型流动分析仪,测试模型采用有机玻璃材质的矩形平板结构;而在湍流边界层猝发频率检测中,则采用了一套基于Mu-level法的湍流猝发频率...  相似文献   

5.
针对某静音型电源车车舱结构及其通风散热特点,建立了车舱内部计算流体力学(Computational Fluid Dynamics,CFD)仿真模型,通过设置各类解析条件,分别利用Standardk-ε,Realizablek-ε,Standardk-ω和SSTk-ω四种湍流模型仿真模拟了车舱内流场和车载柴油发电机组的温度场,并分别测试了两条垂直线的风速对流场仿真结果进行了评价,测试了柴油发电机组和消声器不同测点的温度值,分析了散热的仿真精度.结果表明:k-ε模型的数值模拟结果比k-ω模型更加贴近实测结果,表明Realizablek-ε模型的仿真精度最高,适合静音型电源车车舱结构.  相似文献   

6.
为了研究和优化半封闭倾斜射流中击移动平板的传热性能,采用iSIGHT与CFD软件的联合仿真,根据多岛遗传算法动态调整射流角度和平板移动速度,进行狭缝湍流冲击射流的数值模拟.结果表明,平板表面的传热效果主要是由板速决定的,低速时高角度下的平板表面的平均努塞尔数较高;初始设计时流场左侧的回流区和二次回流区消失,优化后的流场结构得到改善,移动平板表面的平均努塞尔数比初始设计结果提高7.62%,热传导更加均匀.  相似文献   

7.
为验证FINE/Turbo软件对高压涡轮流热耦合求解问题的准确性,将Mark Ⅱ型燃气涡轮叶片作为分析对象,选用不同的湍流模型和转捩模型进行数值模拟,得到叶片表面压力分布,B2B面的压力、温度、马赫数和湍流动能分布,叶片内部温度分布以及叶片表面传热系数分布,并与试验数据进行比较.结果表明:对于流热耦合问题,FINE/T...  相似文献   

8.
针对现代民用飞机设计巡航阻力预测中不考虑转捩影响很难完善计算与试验对比的问题,采用固定转捩和全湍流方法完成DLR_F4翼身组合体阻力计算,并与试验及相关文献结果进行对比.结果表明:采用设置有小范围层流区的固定转捩计算与相应全湍流计算得到的压力因数分布基本一致,二者之间总阻力的差量主要表现在黏性阻力方面;在大多数迎角下,...  相似文献   

9.
本文利用商用CFD软件对压气机转子通流部分建立了一个三维的数值模拟计算平台.对NASA Rotor 37跨音速压气机转子全工况特性进行了计算,与NASA Rotor37的实验结果对比表明,本文的网格生成技术和数值模拟方法都是比较成功的,满足一定的数值求解精度,具有工程技术应用价值.在湍流模型方面引入Baldwin-Lonax(B-L)湍流模型和Spalart-All-maras(S-A)湍流模型,并对模拟结果进行了分析对比研究.对跨音速压气机转子内流场的数值模拟结果表明:S-A湍流模型对跨音速压气机转子的模拟能力优于B-L湍流模型.  相似文献   

10.
在气相湍流流动的k-ε模型基础上,建立了颗粒动力学与湍动能耦合的稠密两相流动数学模型。颗粒相的有效粘性系数取决于颗粒之间相互碰撞而引起的层流粘性以及颗粒微团的湍流脉动而形成的湍流粘性,其中颗粒的碰撞行为以及所形成的颗粒的层流特性用颗粒动力学模型来描述,颗粒的湍流特性采用颗粒湍动能输运方程模型来描述。利用所建立的模型对提升管内气固两相流动过程进行了数值模拟,可以合理地预报出提升管内气固两相的环核流动结构。  相似文献   

11.
Grid model construction is one of the preconditions for computational fluid dynamics (CFD) simulation. As many environmental accidents or unfavorable incidents occur in complex real terrain circumstances, corresponding grid model generation algorithm for scenario simulation has become a hot research field. The digital elevation model (DEM) is common for three-dimensional terrain modeling. DEM data usually consist of a certain number of geodetic coordinates, however, CFD preprocessing platform can't identify geodetic coordinates directly. In this paper, firstly an algorithm of coordinate transformation was proposed, which could convert geodetic coordinates to Cartesian coordinates in the form of length (x), width (y) and height (z). Secondly, another algorithm that generates a complex real terrain grid model was recommended based on the algorithm mentioned previously, which could import converted terrain data into a gridding platform for constructing the CFD terrain grid model. Experiments’ results showed that the terrain grid algorithm obtained through the combination of the two algorithms is highly geometrically consistent with real terrain. The algorithm provided by this study could give a more reliable and convenient basis for the application of CFD fine simulation in real complex terrain.  相似文献   

12.
In the development of products involving fluids, computational fluid dynamics (CFD) has been increasingly applied to investigate the flow associated with various product operating conditions or product designs. The batch simulation is usually conducted when CFD is heavily used, which is not able to respond to the changes in flow regime when the fluid domain changes. In order to overcome this defect, a rule-based intelligent CFD simulation system for steam simulation is proposed to analyze the specific product design and generate the corresponding robust simulation model with accurate results. The rules used in the system are based on physical knowledge and CFD best practices which make this system easy to be applied in other application scenarios by changing the relevant knowledge base. Fluid physics features and dynamic physics features are used to model the intelligent functions of the system. Incorporating CAE boundary features, the CFD analysis view is fulfilled, which maintains the information consistency in a multi-view feature modeling environment. The prototype software tool is developed by Python 3 with separated logics and settings. The effectiveness of the proposed system is proven by the case study of a disk-type gate valve and a pipe reducer in a piping system.  相似文献   

13.
This paper presents a novel modeling approach of coupling transient computational fluid dynamics (CFD) simulation with system identification for control system involving fluid flow and heat transfer. In order to illuminate the feasibility of this method, a fluid flow and heat transfer related process, i.e. a three dimension (3-D) spatio-temporal air temperature distribution and input (inlet air temperature) dependent process in the desert climate chamber, is considered. The distributed parameter models of the chamber temperature are identified using transient CFD simulation results and are then validated against the results obtained from the CFD simulations with high RT2 (more than 0.97) and negative Young’s information criterion (YIC, less than ?11.8). The PI controllers embedded in CFD simulation are then developed based on the models. The performance of the closed-loop systems is also evaluated within the full-scale CFD model. The results show that CFD-based system identification is feasible to model fluid flow and heat transfer related processes.  相似文献   

14.
介绍新型的电厂烟气脱硫仿真系统,提出采用基于CFD模型及过程模型的协同仿真方法进行建模,硬件系统采用虚拟DCS仿真方式.采用CFD方法建立详尽描述吸收塔特性的CFD模型,同时采用集中参数法对FGD其它设备进行建模,协同仿真方法能充分发挥两种建模方法的优点,更精确地描述FGD系统的特性.采用基于虚拟DCS的激励式仿真方法建立仿真系统,结合了全模拟模式和全激励模式的优点,使用虚拟DCS复现实际DCS的全部功能,具有极高的软件逼真度,同时以软件代替部分硬件,可极大地降低实现成本.基于虚拟DCS的电厂烟气脱硫协同仿真系统对于电厂脱硫系统人员培训、运行分析及系统优化研究具有重要作用.  相似文献   

15.
商业CFD程序已广泛应用于反应堆的热工水力模拟,但不能完全满足反应堆的应用需求;开源CFD程序有部分应用,但与商业CFD程序相比,在物理模型全面性、计算精度、计算效率及易用性等方面仍存在差距。为更好地满足局部精细热工水力分析的需求,需要更全面的物理模型、较高的计算精度和较好的并行计算效率,因此有必要开发自主热工CFD程序。详细描述了热工流体力学并行应用程序YH-ACT的设计、实现方案以及测试结果。选取3个典型案例,通过与典型商业软件Fluent计算结果进行对比验证软件正确性, 程序并行计算规模达到400个结点共9 600个进程,稳态计算加速比为111.7,并行效率为27.9%,瞬态计算加速比为37.2,并行效率为9.3%。  相似文献   

16.
This paper describes a complete six-degree-of-freedom nonlinear mathematical model of a tilt rotor unmanned aerial vehicle (UAV). The model is specifically tailored for the design of a hover to forward flight and forward flight to hover transition control system. In that respect, the model includes the aerodynamic effect of propeller-induced airstream which is a function of cruise speed, tilt angle and angle of attack. The cross-section area and output velocity of the propeller-induced airstream are calculated with momentum theory. The projected area on the UAV body that is affected by the propeller-induced airstream is specified and 2D aerodynamic analyses are performed for the airfoil profile of this region. Lookup-tables are generated and implemented in the nonlinear mathematical model. In addition, aerodynamic coefficients of the airframe are calculated by using CFD method and these data are embedded into the nonlinear model as a lookup-table form. In the transition flight regime, both aerodynamic and thrust forces act on the UAV body and the superimposed dynamics become very complex. Hence, it is important to define a method for hover-to-cruise and cruise-to-hover transitions. To this end, both transition scenarios are designed and a state-schedule is developed for flight velocity, angle of attack, and thrust levels of each of the thrust-propellers. This transition state schedule is used as a feedforward state for the flight control system. We present the simulation results of the transition control system and show the successful transition of TURAC in experiment.  相似文献   

17.
针对50公斤级便携式自主水下机器人(AUV)的精确控制和研究,本文介绍了一种基于计算流体力学(CFD)和非线性最优化辨识的动力学建模方法.着重推导了便携式AUV动力学模型,并使用计算流体力学方法代替水池实验获取辨识所需数据和通过非线性最优化方法获得合适的模型结构和模型参数.最终建立了便携式AUV数学模型,并通过对仿真数据与试验数据的对比,证明了该模型及方法的有效性.  相似文献   

18.
张健  周乃春  李明  刘杰  陈江涛  向栋  金韬 《软件学报》2022,33(5):1529-1550
工业CFD (computational fluid dynamics)软件属于计算机辅助工程(computer-aidedengineering, CAE)软件的一种,在航空航天等领域有着广泛的应用.其开发过程强烈依赖于流体力学、数学、计算机以及其他领域学科知识模型,涉及大量理论推导、模型构建、算法优化、验证与确认等专业性、基础性科学研究,导致软件系统构成复杂,研发难度巨大.通过引入软件工程的方法和实践,能够对软件开发进行更有效的组织与管理,达到缩短开发周期、提升软件质量的目的.分析了工业CFD软件的特点和发展趋势,提出了适合于工业CFD软件的增量与迭代结合的开发模型.自主研发了面向CFD仿真软件的自动化持续集成平台.从软件交互、封装与效率、功能扩展性及高性能集群环境部署等方面给出了工业CFD软件的设计建议.针对性建立了适用于科学计算软件的验证与确认方法.最后给出了一款国产自主CFD软件示范性案例,以期为相关研究者和实践者提供参考.  相似文献   

19.
The simulation of the wind action over the CAARC (Commonwealth Advisory Aeronautical Council) standard tall building model is performed in the present work. Aerodynamic and aeroelastic analyses are reproduced numerically in order to demonstrate the applicability of CFD techniques in the field of wind engineering. A major topic in this paper is referred to one of the first attempts to simulate the aeroelastic behavior of a tall building employing complex CFD techniques. Numerical results obtained in this work are compared with numerical and wind tunnel measurements and some important concluding remarks about the present simulation are also reported.  相似文献   

20.
为了掌握乙烯炉炉膛内的热场分布规律,本文采用CFD方法对SL-Ⅱ型工业乙烯裂解炉辐射段内所发生的燃烧、辐射传热、烟气流动等过程进行了耦合模拟,并且详细地分析了炉膛内流场及温度场的分布情况。其中,裂解炉的几何模型按照工程图纸1:1的比例建立;网格划分在专业网格生成软件ICEM11.0中完成;计算采用标准k-ε双方程模型模拟湍流,漩涡耗散/有限速率燃烧反应模型(EDM/FRC)模拟侧壁烧嘴的预混燃烧和底部烧嘴的非预混燃烧,离散传递模型(DTM)模拟炉膛辐射传热,计算过程在CFX5.0中完成。计算得到了裂解炉炉膛内流场、温度场分布的详细信息,模拟结果与工业实测数据吻合较好。模拟结果表明,在底部烧嘴的射流核心区周围形成了大范围的回流,过渡段拐角处有小范围的回流现象;炉膛长度、宽度、高度方向都存在明显的温度梯度,说明传统的炉膛传热计算方法假定温度分布均匀是不准确的;炉膛的高温区主要集中在炉高4.5 m处;炉膛上部的热量,由于侧壁烧嘴的加入而得到了很好地补充,说明侧壁烧嘴的安装位置合理。研究结果表明CFD模拟是目前为止研究裂解炉内热场分布规律最为有效的手段之一,对于未来乙烯裂解炉的设计与优化作用很大。  相似文献   

设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号