用新的多维时间谐波平衡法模拟索引和时钟

IF 1.3 Q2 ENGINEERING, AEROSPACE International Journal of Turbomachinery, Propulsion and Power Pub Date : 2024-05-08 DOI:10.3390/ijtpp9020017
L. Junge, Christian Frey, G. Ashcroft, E. Kügeler
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引用次数: 0

摘要

除了模拟转子-定子相互作用的能力之外,开发涡轮机械流动频域方法的一个核心方面是该方法能够准确预测单通道域上转子-转子和定子-定子之间的相互作用。为了模拟这种相互作用,最先进的频域方法需要一个基本的叶片间相位角,因此有必要采用多通道配置。其他方法则忽略了不同谐波的交叉耦合。因此,无法捕捉到分度对非稳定性干扰传播的影响。为了克服这些问题,作者最近推出了基于时间多维傅里叶变换的谐波平衡方法,并在本研究中进行了扩展,以考虑单通道域上的任意叶片间相角比。为了评估该方法模拟分度对流动的稳定和非稳定部分的影响的能力,在非均质流入条件的影响下,将拟议的扩展应用于民用航空发动机的现代低压风扇级。结果与时域非稳态模拟和基于一维离散傅里叶变换的先进频域方法进行了比较。
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Simulation of Indexing and Clocking with a New Multidimensional Time Harmonic Balance Approach
Alongside the capability to simulate rotor–stator interactions, a central aspect within the development of frequency-domain methods for turbomachinery flows is the ability of the method to accurately predict rotor–rotor and stator–stator interactions on a single-passage domain. To simulate such interactions, state-of-the-art frequency-domain approaches require one fundamental interblade phase angle, and therefore it can be necessary to resort to multi-passage configurations. Other approaches neglect the cross-coupling of different harmonics. As a consequence, the influence of indexing on the propagation of the unsteady disturbances is not captured. To overcome these issues, the harmonic balance approach based on multidimensional Fourier transforms in time, recently introduced by the authors, is extended in this work to account for arbitrary interblade phase angle ratios on a single-passage domain. To assess the ability of the approach to simulate the influence of indexing on the steady, as well as on the unsteady, part of the flow, the proposed extension is applied to a modern low-pressure fan stage of a civil aero engine under the influence of an inhomogeneous inflow condition. The results are compared to unsteady simulations in the time-domain and to state-of-the-art frequency-domain methods based on one-dimensional discrete Fourier transforms.
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来源期刊
CiteScore
2.30
自引率
21.40%
发文量
29
审稿时长
11 weeks
期刊最新文献
Turbofan Performance Estimation Using Neural Network Component Maps and Genetic Algorithm-Least Squares Solvers Experimental Investigation of an Efficient and Lightweight Designed Counter-Rotating Shrouded Fan Stage Experimental Investigation of the Sensitivity of Forced Response to Cold Streaks in an Axial Turbine Heat Load Development and Heat Map Sensitivity Analysis for Civil Aero-Engines Numerical Investigation of Forced Response in a Transonic Compressor Stage—Highlighting Challenges Using Experimental Validation
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