双涵道叶轮机S2流面反问题计算方法

在双涵道叶轮机风扇和压气机的设计中,本文将风扇及内外涵叶片的S2流面反问题统一起来,而成为一个统一的双涵道叶轮机S2流面反问题.在分涵处,采用一列重叠网格,用来传递分涵处上游和下游的流场信息,分流机匣最前面的点既是内涵的计算点,又是外涵的计算点,以该点的压力值作为收敛的判断依据,通过改变分流比,使计算得到的两个压力值相等,分流机匣前的流线平滑,从而得到合适的流场.本方法适用于较复杂的双涵道叶轮机设计,风扇和内外涵叶片排数理论上都不受限制.     

风扇/增压级非设计工况特性分析

本文对某涡扇发动机风扇-外涵道-内涵道整体进行三维定常数值模拟,对内外涵道在设计转速下的流量特性和非设计工况下的气动性能进行了分析。得到内外涵道的稳定工作区域以及在内外涵道堵塞和近失速点的流场信息,为风扇／增压级整体结构的性能评估和优化设计提供了一定的依据。     

变循环核心压气机可调特性的数值研究

利用三维数值工具对某变循环核心压机在设计转速下内、外涵节流特性进行了模拟,分析了核心机驱动风扇级、高压压气机以及二级涵道的工作特点和匹配关系,分析了变循环核心压气机的可调极限。研究结果表明,外涵道节流可以实现涵道比的大范围调节(0.243~0.062),内涵道节流可以实现总增压比的大范围调节(0.81~1.13倍设计压比)。二级涵道出口导向叶片的失速和核心机驱动风扇级的堵塞决定了外涵道节流的可调极限,高压压气机的失速和堵塞决定了内涵道节流的可调极限。     

跨声速风扇流场中弯叶片抗畸变能力研究

采用全流道三维非定常数值模拟的方法研究了进口总压畸变条件下静叶弯叶片对跨声速风扇流场的影响,给出了静叶弯曲对风扇流场的改善情况.重点分析了不同叶高处动静叶流场的变化情况.     

模式选择阀开度对变循环压缩系统匹配的影响

对双外涵变循环压缩系统进行了建模和全三维数值模拟,分析了模式转换过程中第二外涵道倒流对系统气动性能及部件匹配规律的影响。随着倒流流量的增大,变循环压缩系统的第一外涵道比和总涵道比提高,风扇总压比升高,CDFS与高压压气机的总压比降低。倒流主要影响风扇后面级的气动性能。倒流导致CDFS进口流场发生畸变,CDFS下游第一分流环局部流场严重恶化,应及时调节系统控制参数防止压缩系统失效。     

Magnus效应动力演示仪

自制实验装置演示了Magnus效应,3D打印转子,转涵道风扇模拟自然风,遥控转速和风速控制Magnus力.采用控制变量法研究了风速、转速以及压力的关系.实验结果表明:当风速或者转速增加到一定程度,压力反而会减小.     

多级风扇/压气机三维粘性流场的数值分析

采用叶排间掺混面模型,研究了多级跨音速风扇及压气机三维粘性流动数值模拟问题,利用ＬＵ－ＳＧＳ隐式算法使计算过程快速收敛,通过高分辨率格式改善跨音速流场中激波的分辨率。对某双级跨音速风扇及五级压气机流场进行了计算,双级风扇各状态的计算结果与实验数据吻合较好。     

轴向超音来流风扇转子流场数值模拟

本文根据轴向超音来流风扇流动特点,给出其流场数值模拟的边界条件,并依据出口流动状况对计算域提出相应要求,对两种轴向超音来流风扇转于内流动进行了数值模拟。     

某跨音风扇转子全三维设计与数值模拟

本文采用与三维流场分析程序相匹配的任意叶轮机通用叶片造型程序,进行某单级高通流、跨音、宽弦长风扇转子设计。在设计过程中,通过调整转子进口流量、出口总压、叶片最大相对厚度和前后缘厚度等参数沿径向的分布,弯度和最大弯度位置沿弦向的分布,从设计上减弱了叶片上部的激波强度、降低了激波及其关联的损失,克服了该转子叶尖高相对马赫数和低损失、高效率的矛盾。最终获得满足气动性能和结构强度的风扇转子.     

轴流压气机转子叶片的流固耦合分析

本文针对压气机转子叶片流固耦合问题,采用耦合平台MpCCI连接商业CFD软件FINE/Turbo与CSM软件ABAQUS模拟了设计转速下不同流量工况点的流固耦合问题,对比了流场定常计算与流固耦合非定常计算的结果,得到了叶片振动位移频谱振幅图以及效率和压比变化曲线。研究结果表明在失速点附近叶片振动对流场有显著影响,由此可以对压气机的颤振问题进行预测。     

离心压气机级三元粘性计算

使用叶片排间隙混合平面概念，完成离心压气机级多叶片排三元N-S方程计算。每个动静叶片排内的流动被认为是定常的且由相对独立的程序段进行运算。这样的串行程序很容易被改造为在并行系统上运行的SPMD并行程序。     

Numerical and experimental investigations of the unsteady aerodynamics and aero-acoustics characteristics of a backward curved blade centrifugal fan

A numerical study of the aerodynamic and aeroacoustic behaviors of a backward curved blade centrifugal fan was conducted under two important flow conditions: BEP and 1.3 × BEP. Three-dimensional numerical simulations of the complete unsteady flow field for the whole impeller-volute configuration were used to determine the aeroacoustic sources. To locate the unsteady flow and perturbations, the near field wall pressure fluctuations at different strategic points on the volute were computed using the URANS approach. Thus the intensities and positions of the aeroacoustic sources were identified by analyzing frequency spectra. The aeroacoustic sources caused by fluctuations in the interactions of the flows leaving the impeller and volute were close to the volute tongue, and the most effective noise sources related to the flow rate were near the impeller shrouds. In addition, the unsteady flow variables provided by CFD calculations were used as inputs in the Ffowcs Williams-Hawkings equation to estimate the noise tones of the fan. The aeroacoustic calculation results showed that the volute noise was much larger than the blade noise, and the noise mainly propagated from the outlet duct of the fan. Moreover, to account for the noise propagation, three calculation methods were used by applying different solid boundaries. Compared with the other methods, the FEM method, which accounted for the complex solid boundaries, produced good agreement and showed that the complex solid boundaries cannot be neglected in aeroacoustic predictions. The calculation results showed good agreement with the experimental results.     

涡轮三维叶栅的气热耦合数值模拟

本文借助数值模拟技术分析了三维跨音速涡轮导向叶栅不同壁面边界条件对流场流动状况的影响,壁面边界分别采用绝热、等温、耦合换热三种条件。通过对计算结果的分析表明,不同叶片表面边界条件对流场温度场有很大影响,对流场内的压力场及其它参数也有明显影响,因此在气冷涡轮设计中使用多场耦合技术进行数值模拟是非常必要的。     

反弯曲扩压时栅降低二次流损失的实验研究

1前言近年来，压气机叶栅中应用弯曲叶片的研究已受到许多学者的重视l‘，‘］并得到了一些有益的结果。我们已完成的正倾斜、正弯曲和S型平面扩压叶棚的实验结果也表明，采用正弯曲方式的叶片可明显改善叶栅根区气流流动状况，延缓壁角失速，降低端区二次流损失【‘，‘1。为了对比在相同的叶片倾斜角下不同叶片堆迭线型式对叶栅流场的影响，进行了应用反弯曲叶片的压气机平面叶栅的实验研究，以期找出比较合理的叶片弯曲型式，从而降低叶栅的二次流损失。本文在0”、土5”和土10“冲角下，对叶片堆送线如图1所示的反弯曲叶片组成的扩压叶…     

使用流道反算延伸的多叶片排并行计算

计算域延伸与否对多叶片排计算模式的发展起到了很大的作用。计算域的延伸除了起到使计算域重叠,以便相邻叶片排能相互提供确定应力分布的作用外;还使计算域进出气边远离叶片前后缘,以减少边界反射引起的附加误差。并减少交接边界上周向不均匀性引起的掺混损失。本文探索进行适量延伸,以便在重叠区计算确定应力;不进行背压调整。使用确定应力模型的多叶片排并行计算新的途径。     

汽轮机次、末两级弯扭静叶的工程设计与实验研究

本文的主要目的是讨论弯扭叶片在大功率汽轮机低压缸末级和次东级的工程应用问题。具有弯扭叶片的通流设计方法采用基于求解欧拉方程的Ｓ２流面正问题计算，静叶栅的实验是在环形叶栅实验风洞上进行的，通过对计算结果和实验结果的分析，本文讨论了弯扭叶片在次、末两级中对改善流场的作用。     

A numerical study on the flow and sound fields of centrifugal impeller located near a wedge

Centrifugal fans are widely used and the noise generated by these machines causes one of the serious problems. In general, the centrifugal fan noise is often dominated by tones at blade passage frequency and its higher harmonics. This is a consequence of the strong interaction between the flow discharged from the impeller and the cut-off in the casing. However, only a few researches have been carried out on predicting the noise because of the difficulty in obtaining detailed information about the flow field and considering the scattering effect of the casing. The objective of this study is to understand the generation mechanism of sound and to develop a prediction method for the unsteady flow field and the acoustic pressure field of the centrifugal impeller. A discrete vortex method is used to model the centrifugal impeller and a wedge and to calculate the flow field. The force of each element on the blade is calculated by the unsteady Bernoulli equation. Lowson's method is used to predict the acoustic source. In order to consider the scattering and diffraction effects of the casing, Kirchhoff-Helmholtz boundary element method (BEM) is developed. The source of Kirchhoff-Helmholtz BEM is newly developed, so the sound field of the centrifugal fan can be obtained. A centrifugal impeller and wedge are used in the numerical calculation and the results are compared with the experimental data. Reasonable results are obtained not only for the peak frequencies but also for the amplitudes of the tonal sound. The radiated acoustic field shows the diffraction and scattering effect of the wedge.     

涡轮叶栅气热耦合数值模拟

本文建立了透平机械叶栅流场与叶片温度场的气热耦合计算模型,编制了三维非正交曲线坐标系下的温度场求解程序,计算了实心及空心叶片的温度场分布。介绍了区域分解方法在耦合计算及并行计算中的应用,以矩形区域温度场求解程序为例研究了程序的并行化,最后进仃了叶栅流场计算与叶片导热计算程序的分区耦合计算。